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1 | /*#######################################################################################*/ |
1 | /*#######################################################################################*/ |
2 | /* !!! THIS IS NOT FREE SOFTWARE !!! */ |
2 | /* !!! THIS IS NOT FREE SOFTWARE !!! */ |
3 | /*#######################################################################################*/ |
3 | /*#######################################################################################*/ |
4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
4 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
5 | // + www.MikroKopter.com |
5 | // + www.MikroKopter.com |
6 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
6 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
7 | // + Software Nutzungsbedingungen (english version: see below) |
7 | // + Software Nutzungsbedingungen (english version: see below) |
8 | // + der Fa. HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland - nachfolgend Lizenzgeber genannt - |
8 | // + der Fa. HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland - nachfolgend Lizenzgeber genannt - |
9 | // + Der Lizenzgeber räumt dem Kunden ein nicht-ausschließliches, zeitlich und räumlich* unbeschränktes Recht ein, die im den |
9 | // + Der Lizenzgeber räumt dem Kunden ein nicht-ausschließliches, zeitlich und räumlich* unbeschränktes Recht ein, die im den |
10 | // + Mikrocontroller verwendete Firmware für die Hardware Flight-Ctrl, Navi-Ctrl, BL-Ctrl, MK3Mag & PC-Programm MikroKopter-Tool |
10 | // + Mikrocontroller verwendete Firmware für die Hardware Flight-Ctrl, Navi-Ctrl, BL-Ctrl, MK3Mag & PC-Programm MikroKopter-Tool |
11 | // + - nachfolgend Software genannt - nur für private Zwecke zu nutzen. |
11 | // + - nachfolgend Software genannt - nur für private Zwecke zu nutzen. |
12 | // + Der Einsatz dieser Software ist nur auf oder mit Produkten des Lizenzgebers zulässig. |
12 | // + Der Einsatz dieser Software ist nur auf oder mit Produkten des Lizenzgebers zulässig. |
13 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
13 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
14 | // + Die vom Lizenzgeber gelieferte Software ist urheberrechtlich geschützt. Alle Rechte an der Software sowie an sonstigen im |
14 | // + Die vom Lizenzgeber gelieferte Software ist urheberrechtlich geschützt. Alle Rechte an der Software sowie an sonstigen im |
15 | // + Rahmen der Vertragsanbahnung und Vertragsdurchführung überlassenen Unterlagen stehen im Verhältnis der Vertragspartner ausschließlich dem Lizenzgeber zu. |
15 | // + Rahmen der Vertragsanbahnung und Vertragsdurchführung überlassenen Unterlagen stehen im Verhältnis der Vertragspartner ausschließlich dem Lizenzgeber zu. |
16 | // + Die in der Software enthaltenen Copyright-Vermerke, Markenzeichen, andere Rechtsvorbehalte, Seriennummern sowie |
16 | // + Die in der Software enthaltenen Copyright-Vermerke, Markenzeichen, andere Rechtsvorbehalte, Seriennummern sowie |
17 | // + sonstige der Programmidentifikation dienenden Merkmale dürfen vom Kunden nicht verändert oder unkenntlich gemacht werden. |
17 | // + sonstige der Programmidentifikation dienenden Merkmale dürfen vom Kunden nicht verändert oder unkenntlich gemacht werden. |
18 | // + Der Kunde trifft angemessene Vorkehrungen für den sicheren Einsatz der Software. Er wird die Software gründlich auf deren |
18 | // + Der Kunde trifft angemessene Vorkehrungen für den sicheren Einsatz der Software. Er wird die Software gründlich auf deren |
19 | // + Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
19 | // + Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
20 | // + Die Haftung des Lizenzgebers wird - soweit gesetzlich zulässig - begrenzt in Höhe des typischen und vorhersehbaren |
20 | // + Die Haftung des Lizenzgebers wird - soweit gesetzlich zulässig - begrenzt in Höhe des typischen und vorhersehbaren |
21 | // + Schadens. Die gesetzliche Haftung bei Personenschäden und nach dem Produkthaftungsgesetz bleibt unberührt. Dem Lizenzgeber steht jedoch der Einwand |
21 | // + Schadens. Die gesetzliche Haftung bei Personenschäden und nach dem Produkthaftungsgesetz bleibt unberührt. Dem Lizenzgeber steht jedoch der Einwand |
22 | // + des Mitverschuldens offen. |
22 | // + des Mitverschuldens offen. |
23 | // + Der Kunde trifft angemessene Vorkehrungen für den Fall, dass die Software ganz oder teilweise nicht ordnungsgemäß arbeitet. |
23 | // + Der Kunde trifft angemessene Vorkehrungen für den Fall, dass die Software ganz oder teilweise nicht ordnungsgemäß arbeitet. |
24 | // + Er wird die Software gründlich auf deren Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
24 | // + Er wird die Software gründlich auf deren Verwendbarkeit zu dem von ihm beabsichtigten Zweck testen, bevor er diese operativ einsetzt. |
25 | // + Der Kunde wird er seine Daten vor Einsatz der Software nach dem Stand der Technik sichern. |
25 | // + Der Kunde wird er seine Daten vor Einsatz der Software nach dem Stand der Technik sichern. |
26 | // + Der Kunde ist darüber unterrichtet, dass der Lizenzgeber seine Daten im zur Vertragsdurchführung erforderlichen Umfang |
26 | // + Der Kunde ist darüber unterrichtet, dass der Lizenzgeber seine Daten im zur Vertragsdurchführung erforderlichen Umfang |
27 | // + und auf Grundlage der Datenschutzvorschriften erhebt, speichert, verarbeitet und, sofern notwendig, an Dritte übermittelt. |
27 | // + und auf Grundlage der Datenschutzvorschriften erhebt, speichert, verarbeitet und, sofern notwendig, an Dritte übermittelt. |
28 | // + *) Die räumliche Nutzung bezieht sich nur auf den Einsatzort, nicht auf die Reichweite der programmierten Software. |
28 | // + *) Die räumliche Nutzung bezieht sich nur auf den Einsatzort, nicht auf die Reichweite der programmierten Software. |
29 | // + #### ENDE DER NUTZUNGSBEDINGUNGEN ####' |
29 | // + #### ENDE DER NUTZUNGSBEDINGUNGEN ####' |
30 | // + Hinweis: Informationen über erweiterte Nutzungsrechte (wie z.B. Nutzung für nicht-private Zwecke) sind auf Anfrage per Email an info(@)hisystems.de verfügbar. |
30 | // + Hinweis: Informationen über erweiterte Nutzungsrechte (wie z.B. Nutzung für nicht-private Zwecke) sind auf Anfrage per Email an info(@)hisystems.de verfügbar. |
31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
31 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
32 | // + Software LICENSING TERMS |
32 | // + Software LICENSING TERMS |
33 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
33 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
34 | // + of HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland, Germany - the Licensor - |
34 | // + of HiSystems GmbH, Flachsmeerstrasse 2, 26802 Moormerland, Germany - the Licensor - |
35 | // + The Licensor grants the customer a non-exclusive license to use the microcontroller firmware of the Flight-Ctrl, Navi-Ctrl, BL-Ctrl, and MK3Mag hardware |
35 | // + The Licensor grants the customer a non-exclusive license to use the microcontroller firmware of the Flight-Ctrl, Navi-Ctrl, BL-Ctrl, and MK3Mag hardware |
36 | // + (the Software) exclusively for private purposes. The License is unrestricted with respect to time and territory*. |
36 | // + (the Software) exclusively for private purposes. The License is unrestricted with respect to time and territory*. |
37 | // + The Software may only be used with the Licensor's products. |
37 | // + The Software may only be used with the Licensor's products. |
38 | // + The Software provided by the Licensor is protected by copyright. With respect to the relationship between the parties to this |
38 | // + The Software provided by the Licensor is protected by copyright. With respect to the relationship between the parties to this |
39 | // + agreement, all rights pertaining to the Software and other documents provided during the preparation and execution of this |
39 | // + agreement, all rights pertaining to the Software and other documents provided during the preparation and execution of this |
40 | // + agreement shall be the property of the Licensor. |
40 | // + agreement shall be the property of the Licensor. |
41 | // + The information contained in the Software copyright notices, trademarks, other legal reservations, serial numbers and other |
41 | // + The information contained in the Software copyright notices, trademarks, other legal reservations, serial numbers and other |
42 | // + features that can be used to identify the program may not be altered or defaced by the customer. |
42 | // + features that can be used to identify the program may not be altered or defaced by the customer. |
43 | // + The customer shall be responsible for taking reasonable precautions |
43 | // + The customer shall be responsible for taking reasonable precautions |
44 | // + for the safe use of the Software. The customer shall test the Software thoroughly regarding its suitability for the |
44 | // + for the safe use of the Software. The customer shall test the Software thoroughly regarding its suitability for the |
45 | // + intended purpose before implementing it for actual operation. The Licensor's liability shall be limited to the extent of typical and |
45 | // + intended purpose before implementing it for actual operation. The Licensor's liability shall be limited to the extent of typical and |
46 | // + foreseeable damage to the extent permitted by law, notwithstanding statutory liability for bodily injury and product |
46 | // + foreseeable damage to the extent permitted by law, notwithstanding statutory liability for bodily injury and product |
47 | // + liability. However, the Licensor shall be entitled to the defense of contributory negligence. |
47 | // + liability. However, the Licensor shall be entitled to the defense of contributory negligence. |
48 | // + The customer will take adequate precautions in the case, that the software is not working properly. The customer will test |
48 | // + The customer will take adequate precautions in the case, that the software is not working properly. The customer will test |
49 | // + the software for his purpose before any operational usage. The customer will backup his data before using the software. |
49 | // + the software for his purpose before any operational usage. The customer will backup his data before using the software. |
50 | // + The customer understands that the Licensor collects, stores and processes, and, where required, forwards, customer data |
50 | // + The customer understands that the Licensor collects, stores and processes, and, where required, forwards, customer data |
51 | // + to third parties to the extent necessary for executing the agreement, subject to applicable data protection and privacy regulations. |
51 | // + to third parties to the extent necessary for executing the agreement, subject to applicable data protection and privacy regulations. |
52 | // + *) The territory aspect only refers to the place where the Software is used, not its programmed range. |
52 | // + *) The territory aspect only refers to the place where the Software is used, not its programmed range. |
53 | // + #### END OF LICENSING TERMS #### |
53 | // + #### END OF LICENSING TERMS #### |
54 | // + Note: For information on license extensions (e.g. commercial use), please contact us at info(@)hisystems.de. |
54 | // + Note: For information on license extensions (e.g. commercial use), please contact us at info(@)hisystems.de. |
55 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
55 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
56 | 56 | ||
57 | #include <string.h> |
57 | #include <string.h> |
58 | #include <math.h> |
58 | #include <math.h> |
59 | #include "91x_lib.h" |
59 | #include "91x_lib.h" |
60 | #include "led.h" |
60 | #include "led.h" |
61 | #include "gps.h" |
61 | #include "gps.h" |
62 | #include "uart1.h" |
62 | #include "uart1.h" |
63 | #include "spi_slave.h" |
63 | #include "spi_slave.h" |
64 | #include "compass.h" |
64 | #include "compass.h" |
65 | #include "timer1.h" |
65 | #include "timer1.h" |
66 | #include "timer2.h" |
66 | #include "timer2.h" |
67 | #include "config.h" |
67 | #include "config.h" |
68 | #include "main.h" |
68 | #include "main.h" |
69 | #include "compass.h" |
69 | #include "compass.h" |
70 | #include "params.h" |
70 | #include "params.h" |
71 | #include "stdlib.h" |
71 | #include "stdlib.h" |
72 | #include "settings.h" |
72 | #include "settings.h" |
73 | #include "ncmag.h" |
73 | #include "ncmag.h" |
74 | 74 | ||
75 | #define SPI_RXSYNCBYTE1 0xAA |
75 | #define SPI_RXSYNCBYTE1 0xAA |
76 | #define SPI_RXSYNCBYTE2 0x83 |
76 | #define SPI_RXSYNCBYTE2 0x83 |
77 | #define SPI_TXSYNCBYTE1 0x81 |
77 | #define SPI_TXSYNCBYTE1 0x81 |
78 | #define SPI_TXSYNCBYTE2 0x55 |
78 | #define SPI_TXSYNCBYTE2 0x55 |
79 | 79 | ||
80 | //communication packets |
80 | //communication packets |
81 | FromFlightCtrl_t FromFlightCtrl; |
81 | FromFlightCtrl_t FromFlightCtrl; |
82 | ToFlightCtrl_t ToFlightCtrl; |
82 | ToFlightCtrl_t ToFlightCtrl; |
83 | #define SPI0_TIMEOUT 2500 //ms |
83 | #define SPI0_TIMEOUT 2500 //ms |
84 | volatile u32 SPI0_Timeout = 0; |
84 | volatile u32 SPI0_Timeout = 0; |
85 | u8 Logging_FCStatusFlags1 = 0,Logging_FCStatusFlags2 = 0; |
85 | u8 Logging_FCStatusFlags1 = 0,Logging_FCStatusFlags2 = 0; |
86 | u8 SpeakHoTT = 0; |
86 | u8 SpeakHoTT = 0; |
87 | 87 | ||
88 | // tx packet buffer |
88 | // tx packet buffer |
89 | #define SPI_TXBUFFER_LEN (2 + sizeof(ToFlightCtrl)) // 2 bytes at start are for synchronization |
89 | #define SPI_TXBUFFER_LEN (2 + sizeof(ToFlightCtrl)) // 2 bytes at start are for synchronization |
90 | volatile u8 SPI_TxBuffer[SPI_TXBUFFER_LEN + 10]; |
90 | volatile u8 SPI_TxBuffer[SPI_TXBUFFER_LEN + 10]; |
91 | volatile u8 SPI_TxBufferIndex = 0; |
91 | volatile u8 SPI_TxBufferIndex = 0; |
92 | u8 *Ptr_TxChksum = NULL ; // pointer to checksum in TxBuffer |
92 | u8 *Ptr_TxChksum = NULL ; // pointer to checksum in TxBuffer |
93 | 93 | ||
94 | // rx packet buffer |
94 | // rx packet buffer |
95 | #define SPI_RXBUFFER_LEN sizeof(FromFlightCtrl) |
95 | #define SPI_RXBUFFER_LEN sizeof(FromFlightCtrl) |
96 | volatile u8 SPI_RxBuffer[SPI_RXBUFFER_LEN+10]; |
96 | volatile u8 SPI_RxBuffer[SPI_RXBUFFER_LEN+10]; |
97 | volatile u8 SPI_RxBufferIndex = 0; |
97 | volatile u8 SPI_RxBufferIndex = 0; |
98 | volatile u8 SPI_RxBuffer_Request = 0; |
98 | volatile u8 SPI_RxBuffer_Request = 0; |
99 | #define SPI_COMMAND_INDEX 0 |
99 | #define SPI_COMMAND_INDEX 0 |
100 | 100 | ||
101 | s32 Kalman_K = 32; |
101 | s32 Kalman_K = 32; |
102 | s32 Kalman_MaxDrift = 5 * 16; |
102 | s32 Kalman_MaxDrift = 5 * 16; |
103 | s32 Kalman_MaxFusion = 64; |
103 | s32 Kalman_MaxFusion = 64; |
104 | s32 Kalman_Kompass = 32; |
104 | s32 Kalman_Kompass = 32; |
105 | s32 ToFcGpsZ = 0; |
105 | s32 ToFcGpsZ = 0; |
106 | u8 CompassCalState = 0; |
106 | u8 CompassCalState = 0; |
107 | 107 | ||
108 | u8 SPI_CommandSequence[] = { SPI_NCCMD_KALMAN, SPI_NCCMD_GPSINFO ,SPI_NCCMD_KALMAN, SPI_NCCMD_HOTT_INFO, SPI_NCCMD_KALMAN, SPI_MISC, SPI_NCCMD_KALMAN, SPI_NCCMD_VERSION }; |
108 | u8 SPI_CommandSequence[] = { SPI_NCCMD_KALMAN, SPI_NCCMD_GPSINFO ,SPI_NCCMD_KALMAN, SPI_NCCMD_HOTT_INFO, SPI_NCCMD_KALMAN, SPI_MISC, SPI_NCCMD_KALMAN, SPI_NCCMD_VERSION }; |
109 | u8 SPI_CommandCounter = 0; |
109 | u8 SPI_CommandCounter = 0; |
110 | s32 ToFC_Rotate_C = 64, ToFC_Rotate_S = 0; |
110 | s32 ToFC_Rotate_C = 64, ToFC_Rotate_S = 0; |
111 | s32 HeadFreeStartAngle = 0; |
111 | s32 HeadFreeStartAngle = 0; |
112 | s16 FC_WP_EventChannel = 0, LogFC_WP_EventChannel = 0; // gibt einen Schaltkanal an die FC weiter, wenn der Wegpunkt erreicht wurde |
112 | s16 FC_WP_EventChannel = 0, LogFC_WP_EventChannel = 0; // gibt einen Schaltkanal an die FC weiter, wenn der Wegpunkt erreicht wurde |
113 | u32 ToFC_AltitudeRate = 0; |
113 | u32 ToFC_AltitudeRate = 0; |
114 | s32 ToFC_AltitudeSetpoint = 0; |
114 | s32 ToFC_AltitudeSetpoint = 0; |
115 | u8 FromFC_VarioCharacter = ' '; |
115 | u8 FromFC_VarioCharacter = ' '; |
116 | u8 GPS_Aid_StickMultiplikator = 0; |
116 | u8 GPS_Aid_StickMultiplikator = 0; |
117 | u8 NC_GPS_ModeCharacter = ' '; |
117 | u8 NC_GPS_ModeCharacter = ' '; |
118 | u8 FCCalibActive = 0; |
118 | u8 FCCalibActive = 0; |
119 | u8 FC_is_Calibrated = 0; |
119 | u8 FC_is_Calibrated = 0; |
120 | Motor_t Motor[12]; |
120 | Motor_t Motor[12]; |
121 | u8 Motor_Version[12]; // das kann nicht in die struct, weil der PC die Struktur bekommt |
121 | u8 Motor_Version[12]; // das kann nicht in die struct, weil der PC die Struktur bekommt |
122 | u8 NC_To_FC_Flags = 0; |
122 | u8 NC_To_FC_Flags = 0; |
123 | u8 BL_MinOfMaxPWM; // indication if all BL-controllers run on full power |
123 | u8 BL_MinOfMaxPWM; // indication if all BL-controllers run on full power |
124 | u32 FC_I2C_ErrorConter; |
124 | u32 FC_I2C_ErrorConter; |
125 | SPI_Version_t FC_Version; |
125 | SPI_Version_t FC_Version; |
126 | s16 POI_KameraNick = 0; |
126 | s16 POI_KameraNick = 0; |
127 | u8 NC_Wait_for_LED = 0; |
127 | u8 NC_Wait_for_LED = 0; |
128 | s16 GyroCompassCorrected = 0; // corrected with the magnetic declination |
128 | s16 GyroCompassCorrected = 0; // corrected with the magnetic declination |
129 | 129 | ||
130 | //-------------------------------------------------------------- |
130 | //-------------------------------------------------------------- |
131 | void SSP0_IRQHandler(void) |
131 | void SSP0_IRQHandler(void) |
132 | { |
132 | { |
133 | static u8 rxchksum = 0; |
133 | static u8 rxchksum = 0; |
134 | u8 rxdata; |
134 | u8 rxdata; |
135 | 135 | ||
136 | #define SPI_SYNC1 0 |
136 | #define SPI_SYNC1 0 |
137 | #define SPI_SYNC2 1 |
137 | #define SPI_SYNC2 1 |
138 | #define SPI_DATA 2 |
138 | #define SPI_DATA 2 |
139 | static u8 SPI_State = SPI_SYNC1; |
139 | static u8 SPI_State = SPI_SYNC1; |
140 | //IENABLE; |
140 | //IENABLE; |
141 | 141 | ||
142 | // clear pending bits |
142 | // clear pending bits |
143 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxTimeOut); |
143 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxTimeOut); |
144 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxFifo); |
144 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxFifo); |
145 | 145 | ||
146 | // while RxFIFO not empty |
146 | // while RxFIFO not empty |
147 | while(SSP_GetFlagStatus(SSP0, SSP_FLAG_RxFifoNotEmpty) == SET) |
147 | while(SSP_GetFlagStatus(SSP0, SSP_FLAG_RxFifoNotEmpty) == SET) |
148 | { |
148 | { |
149 | rxdata = SSP0->DR; // catch the received byte |
149 | rxdata = SSP0->DR; // catch the received byte |
150 | // Fill TxFIFO while its not full or end of packet is reached |
150 | // Fill TxFIFO while its not full or end of packet is reached |
151 | while (SSP_GetFlagStatus(SSP0, SSP_FLAG_TxFifoNotFull) == SET) |
151 | while (SSP_GetFlagStatus(SSP0, SSP_FLAG_TxFifoNotFull) == SET) |
152 | { |
152 | { |
153 | if (SPI_TxBufferIndex < SPI_TXBUFFER_LEN) // still data to send ? |
153 | if (SPI_TxBufferIndex < SPI_TXBUFFER_LEN) // still data to send ? |
154 | { |
154 | { |
155 | SSP0->DR = SPI_TxBuffer[SPI_TxBufferIndex]; // send a byte |
155 | SSP0->DR = SPI_TxBuffer[SPI_TxBufferIndex]; // send a byte |
156 | *Ptr_TxChksum += SPI_TxBuffer[SPI_TxBufferIndex]; // update checksum |
156 | *Ptr_TxChksum += SPI_TxBuffer[SPI_TxBufferIndex]; // update checksum |
157 | if(SPIWatchDog == 0) *Ptr_TxChksum += 1; // disturbe this packet to stop the communication! |
157 | if(SPIWatchDog == 0) *Ptr_TxChksum += 1; // disturbe this packet to stop the communication! |
158 | SPI_TxBufferIndex++; // pointer to next byte |
158 | SPI_TxBufferIndex++; // pointer to next byte |
159 | } |
159 | } |
160 | else // end of packet is reached reset and copy data to tx buffer |
160 | else // end of packet is reached reset and copy data to tx buffer |
161 | { |
161 | { |
162 | SPI_TxBufferIndex = 0; // reset buffer index |
162 | SPI_TxBufferIndex = 0; // reset buffer index |
163 | ToFlightCtrl.Chksum = 0; // initialize checksum |
163 | ToFlightCtrl.Chksum = 0; // initialize checksum |
164 | ToFlightCtrl.BeepTime = BeepTime; // set beeptime |
164 | ToFlightCtrl.BeepTime = BeepTime; // set beeptime |
165 | BeepTime = 0; // reset local beeptime |
165 | BeepTime = 0; // reset local beeptime |
166 | // copy contents of ToFlightCtrl->SPI_TxBuffer |
166 | // copy contents of ToFlightCtrl->SPI_TxBuffer |
167 | memcpy((u8 *) &(SPI_TxBuffer[2]), (u8 *) &ToFlightCtrl, sizeof(ToFlightCtrl)); |
167 | memcpy((u8 *) &(SPI_TxBuffer[2]), (u8 *) &ToFlightCtrl, sizeof(ToFlightCtrl)); |
168 | } |
168 | } |
169 | } |
169 | } |
170 | switch (SPI_State) |
170 | switch (SPI_State) |
171 | { |
171 | { |
172 | case SPI_SYNC1: |
172 | case SPI_SYNC1: |
173 | SPI_RxBufferIndex = 0; // reset buffer index |
173 | SPI_RxBufferIndex = 0; // reset buffer index |
174 | rxchksum = rxdata; // init checksum |
174 | rxchksum = rxdata; // init checksum |
175 | if (rxdata == SPI_RXSYNCBYTE1) |
175 | if (rxdata == SPI_RXSYNCBYTE1) |
176 | { // 1st syncbyte ok |
176 | { // 1st syncbyte ok |
177 | SPI_State = SPI_SYNC2; // step to sync2 |
177 | SPI_State = SPI_SYNC2; // step to sync2 |
178 | } |
178 | } |
179 | break; |
179 | break; |
180 | case SPI_SYNC2: |
180 | case SPI_SYNC2: |
181 | if (rxdata == SPI_RXSYNCBYTE2) |
181 | if (rxdata == SPI_RXSYNCBYTE2) |
182 | { // 2nd Syncbyte ok |
182 | { // 2nd Syncbyte ok |
183 | rxchksum += rxdata; |
183 | rxchksum += rxdata; |
184 | SPI_State = SPI_DATA; |
184 | SPI_State = SPI_DATA; |
185 | } // 2nd Syncbyte does not match |
185 | } // 2nd Syncbyte does not match |
186 | else |
186 | else |
187 | { |
187 | { |
188 | SPI_State = SPI_SYNC1; //jump back to sync1 |
188 | SPI_State = SPI_SYNC1; //jump back to sync1 |
189 | } |
189 | } |
190 | break; |
190 | break; |
191 | case SPI_DATA: |
191 | case SPI_DATA: |
192 | SPI_RxBuffer[SPI_RxBufferIndex++]= rxdata; // copy databyte to rx buffer |
192 | SPI_RxBuffer[SPI_RxBufferIndex++]= rxdata; // copy databyte to rx buffer |
193 | if(SPI_RxBufferIndex >= SPI_RXBUFFER_LEN) // end of packet is reached |
193 | if(SPI_RxBufferIndex >= SPI_RXBUFFER_LEN) // end of packet is reached |
194 | { |
194 | { |
195 | if (rxdata == rxchksum) // verify checksum byte |
195 | if (rxdata == rxchksum) // verify checksum byte |
196 | { |
196 | { |
197 | // copy SPI_RxBuffer -> FromFlightCtrl |
197 | // copy SPI_RxBuffer -> FromFlightCtrl |
198 | if(!SPI_RxBuffer_Request) // block writing to FromFlightCtrl on reading access |
198 | if(!SPI_RxBuffer_Request) // block writing to FromFlightCtrl on reading access |
199 | { |
199 | { |
200 | memcpy((u8 *) &FromFlightCtrl, (u8 *) SPI_RxBuffer, sizeof(FromFlightCtrl)); |
200 | memcpy((u8 *) &FromFlightCtrl, (u8 *) SPI_RxBuffer, sizeof(FromFlightCtrl)); |
201 | SPI_RxBuffer_Request = 1; |
201 | SPI_RxBuffer_Request = 1; |
202 | } |
202 | } |
203 | // reset timeout counter on good packet |
203 | // reset timeout counter on good packet |
204 | SPI0_Timeout = SetDelay(SPI0_TIMEOUT); |
204 | SPI0_Timeout = SetDelay(SPI0_TIMEOUT); |
205 | DebugOut.Analog[13]++; |
205 | DebugOut.Analog[13]++; |
206 | } |
206 | } |
207 | else // bad checksum byte |
207 | else // bad checksum byte |
208 | { |
208 | { |
209 | DebugOut.Analog[12]++; // increase SPI chksum error counter |
209 | DebugOut.Analog[12]++; // increase SPI chksum error counter |
210 | } |
210 | } |
211 | SPI_State = SPI_SYNC1; // reset state |
211 | SPI_State = SPI_SYNC1; // reset state |
212 | } |
212 | } |
213 | else // end of packet not reached |
213 | else // end of packet not reached |
214 | { |
214 | { |
215 | rxchksum += rxdata; // update checksum |
215 | rxchksum += rxdata; // update checksum |
216 | } |
216 | } |
217 | break; |
217 | break; |
218 | default: |
218 | default: |
219 | SPI_State = SPI_SYNC1; |
219 | SPI_State = SPI_SYNC1; |
220 | break; |
220 | break; |
221 | } |
221 | } |
222 | } |
222 | } |
223 | 223 | ||
224 | // IDISABLE; |
224 | // IDISABLE; |
225 | VIC1->VAR = 0xFF; // write any value to VIC0 Vector address register |
225 | VIC1->VAR = 0xFF; // write any value to VIC0 Vector address register |
226 | } |
226 | } |
227 | 227 | ||
228 | //-------------------------------------------------------------- |
228 | //-------------------------------------------------------------- |
229 | void SPI0_Init(void) |
229 | void SPI0_Init(void) |
230 | { |
230 | { |
231 | GPIO_InitTypeDef GPIO_InitStructure; |
231 | GPIO_InitTypeDef GPIO_InitStructure; |
232 | SSP_InitTypeDef SSP_InitStructure; |
232 | SSP_InitTypeDef SSP_InitStructure; |
233 | 233 | ||
234 | UART1_PutString("\r\n SPI init..."); |
234 | UART1_PutString("\r\n SPI init..."); |
235 | 235 | ||
236 | SCU_APBPeriphClockConfig(__GPIO2 ,ENABLE); |
236 | SCU_APBPeriphClockConfig(__GPIO2 ,ENABLE); |
237 | SCU_APBPeriphClockConfig(__SSP0 ,ENABLE); |
237 | SCU_APBPeriphClockConfig(__SSP0 ,ENABLE); |
238 | 238 | ||
239 | GPIO_DeInit(GPIO2); |
239 | GPIO_DeInit(GPIO2); |
240 | //SSP0_CLK, SSP0_MOSI, SSP0_NSS pins |
240 | //SSP0_CLK, SSP0_MOSI, SSP0_NSS pins |
241 | GPIO_StructInit(&GPIO_InitStructure); |
241 | GPIO_StructInit(&GPIO_InitStructure); |
242 | GPIO_InitStructure.GPIO_Direction = GPIO_PinInput; |
242 | GPIO_InitStructure.GPIO_Direction = GPIO_PinInput; |
243 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_4 | GPIO_Pin_5 | GPIO_Pin_7; |
243 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_4 | GPIO_Pin_5 | GPIO_Pin_7; |
244 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
244 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
245 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
245 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
246 | GPIO_InitStructure.GPIO_Alternate = GPIO_InputAlt1; //SSP0_SCLK, SSP0_MOSI, SSP0_NSS |
246 | GPIO_InitStructure.GPIO_Alternate = GPIO_InputAlt1; //SSP0_SCLK, SSP0_MOSI, SSP0_NSS |
247 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
247 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
248 | 248 | ||
249 | // SSP0_MISO pin GPIO2.6 |
249 | // SSP0_MISO pin GPIO2.6 |
250 | GPIO_StructInit(&GPIO_InitStructure); |
250 | GPIO_StructInit(&GPIO_InitStructure); |
251 | GPIO_InitStructure.GPIO_Direction = GPIO_PinOutput; |
251 | GPIO_InitStructure.GPIO_Direction = GPIO_PinOutput; |
252 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_6; |
252 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_6; |
253 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
253 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
254 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
254 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
255 | GPIO_InitStructure.GPIO_Alternate = GPIO_OutputAlt2; //SSP0_MISO |
255 | GPIO_InitStructure.GPIO_Alternate = GPIO_OutputAlt2; //SSP0_MISO |
256 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
256 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
257 | 257 | ||
258 | SSP_DeInit(SSP0); |
258 | SSP_DeInit(SSP0); |
259 | SSP_StructInit(&SSP_InitStructure); |
259 | SSP_StructInit(&SSP_InitStructure); |
260 | SSP_InitStructure.SSP_FrameFormat = SSP_FrameFormat_Motorola; |
260 | SSP_InitStructure.SSP_FrameFormat = SSP_FrameFormat_Motorola; |
261 | SSP_InitStructure.SSP_Mode = SSP_Mode_Slave; |
261 | SSP_InitStructure.SSP_Mode = SSP_Mode_Slave; |
262 | SSP_InitStructure.SSP_SlaveOutput = SSP_SlaveOutput_Enable; |
262 | SSP_InitStructure.SSP_SlaveOutput = SSP_SlaveOutput_Enable; |
263 | SSP_InitStructure.SSP_CPHA = SSP_CPHA_1Edge; |
263 | SSP_InitStructure.SSP_CPHA = SSP_CPHA_1Edge; |
264 | SSP_InitStructure.SSP_CPOL = SSP_CPOL_Low; |
264 | SSP_InitStructure.SSP_CPOL = SSP_CPOL_Low; |
265 | SSP_InitStructure.SSP_ClockRate = 0; |
265 | SSP_InitStructure.SSP_ClockRate = 0; |
266 | 266 | ||
267 | SSP_Init(SSP0, &SSP_InitStructure); |
267 | SSP_Init(SSP0, &SSP_InitStructure); |
268 | SSP_ITConfig(SSP0, SSP_IT_RxFifo | SSP_IT_RxTimeOut, ENABLE); |
268 | SSP_ITConfig(SSP0, SSP_IT_RxFifo | SSP_IT_RxTimeOut, ENABLE); |
269 | SSP_Cmd(SSP0, ENABLE); |
269 | SSP_Cmd(SSP0, ENABLE); |
270 | // initialize the syncbytes in the tx buffer |
270 | // initialize the syncbytes in the tx buffer |
271 | SPI_TxBuffer[0] = SPI_TXSYNCBYTE1; |
271 | SPI_TxBuffer[0] = SPI_TXSYNCBYTE1; |
272 | SPI_TxBuffer[1] = SPI_TXSYNCBYTE2; |
272 | SPI_TxBuffer[1] = SPI_TXSYNCBYTE2; |
273 | // set the pointer to the checksum byte in the tx buffer |
273 | // set the pointer to the checksum byte in the tx buffer |
274 | Ptr_TxChksum = (u8 *) &(((ToFlightCtrl_t *) &(SPI_TxBuffer[2]))->Chksum); |
274 | Ptr_TxChksum = (u8 *) &(((ToFlightCtrl_t *) &(SPI_TxBuffer[2]))->Chksum); |
275 | 275 | ||
276 | ToFlightCtrl.GPSStick.Nick = 0; |
276 | ToFlightCtrl.GPSStick.Nick = 0; |
277 | ToFlightCtrl.GPSStick.Roll = 0; |
277 | ToFlightCtrl.GPSStick.Roll = 0; |
278 | // ToFlightCtrl.GPSStick.Yaw = 0; |
278 | // ToFlightCtrl.GPSStick.Yaw = 0; |
279 | 279 | ||
280 | VIC_Config(SSP0_ITLine, VIC_IRQ, PRIORITY_SPI0); |
280 | VIC_Config(SSP0_ITLine, VIC_IRQ, PRIORITY_SPI0); |
281 | VIC_ITCmd(SSP0_ITLine, ENABLE); |
281 | VIC_ITCmd(SSP0_ITLine, ENABLE); |
282 | 282 | ||
283 | SPI0_Timeout = SetDelay(4*SPI0_TIMEOUT); |
283 | SPI0_Timeout = SetDelay(4*SPI0_TIMEOUT); |
284 | 284 | ||
285 | UART1_PutString("ok"); |
285 | UART1_PutString("ok"); |
286 | } |
286 | } |
287 | 287 | ||
288 | 288 | ||
289 | //------------------------------------------------------ |
289 | //------------------------------------------------------ |
290 | void SPI0_UpdateBuffer(void) |
290 | void SPI0_UpdateBuffer(void) |
291 | { |
291 | { |
292 | static u32 timeout = 0; |
292 | static u32 timeout = 0; |
293 | static u8 counter = 50,hott_index = 0, last_error_code = 0, enable_injecting = 0; |
293 | static u8 counter = 50,hott_index = 0, last_error_code = 0, enable_injecting = 0; |
294 | static s16 last_wp_event = 0; |
294 | static s16 last_wp_event = 0; |
295 | s16 tmp; |
295 | s16 tmp; |
296 | s32 i1,i2; |
296 | s32 i1,i2; |
297 | /* |
297 | /* |
298 | union |
298 | union |
299 | { |
299 | { |
300 | unsigned char Byte[4]; |
300 | unsigned char Byte[4]; |
301 | unsigned int Int[2]; |
301 | unsigned int Int[2]; |
302 | unsigned long Long; |
302 | unsigned long Long; |
303 | } Temp; |
303 | } Temp; |
304 | */ |
304 | */ |
305 | SPIWatchDog = 3500; // stop communication to FC after this timeout |
305 | SPIWatchDog = 3500; // stop communication to FC after this timeout |
306 | if(SPI_RxBuffer_Request) |
306 | if(SPI_RxBuffer_Request) |
307 | { |
307 | { |
308 | // avoid sending data via SPI during the update of the ToFlightCtrl structure |
308 | // avoid sending data via SPI during the update of the ToFlightCtrl structure |
309 | VIC_ITCmd(SSP0_ITLine, DISABLE); // disable SPI interrupt |
309 | VIC_ITCmd(SSP0_ITLine, DISABLE); // disable SPI interrupt |
310 | ToFlightCtrl.CompassHeading = Compass_Heading; |
310 | ToFlightCtrl.CompassHeading = Compass_Heading; |
311 | DebugOut.Analog[10] = ToFlightCtrl.CompassHeading; |
311 | DebugOut.Analog[10] = ToFlightCtrl.CompassHeading; |
312 | GyroCompassCorrected = (3600 + FromFlightCtrl.GyroHeading + FC.FromFC_CompassOffset - GeoMagDec) % 3600; |
312 | GyroCompassCorrected = (3600 + FromFlightCtrl.GyroHeading + FC.FromFC_CompassOffset - GeoMagDec) % 3600; |
313 | if(ToFlightCtrl.CompassHeading >= 0) ToFlightCtrl.CompassHeading = (360 + ToFlightCtrl.CompassHeading + FromFlightCtrl.GyroYaw / 12) % 360; |
313 | if(ToFlightCtrl.CompassHeading >= 0) ToFlightCtrl.CompassHeading = (360 + ToFlightCtrl.CompassHeading + FromFlightCtrl.GyroYaw / 12) % 360; |
314 | ToFlightCtrl.MagVecX = MagVector.X; |
314 | ToFlightCtrl.MagVecX = MagVector.X; |
315 | ToFlightCtrl.MagVecY = MagVector.Y; |
315 | ToFlightCtrl.MagVecY = MagVector.Y; |
316 | ToFlightCtrl.MagVecZ = MagVector.Z; |
316 | ToFlightCtrl.MagVecZ = MagVector.Z; |
317 | // ToFlightCtrl.NCStatus = 0; |
317 | // ToFlightCtrl.NCStatus = 0; |
318 | // cycle spi commands |
318 | // cycle spi commands |
319 | if(ErrorCode != last_error_code && enable_injecting) |
319 | if(ErrorCode != last_error_code && enable_injecting) |
320 | { |
320 | { |
321 | ToFlightCtrl.Command = SPI_NCCMD_VERSION; |
321 | ToFlightCtrl.Command = SPI_NCCMD_VERSION; |
322 | last_error_code = ErrorCode; |
322 | last_error_code = ErrorCode; |
323 | enable_injecting = 0; |
323 | enable_injecting = 0; |
324 | } |
324 | } |
325 | else |
325 | else |
326 | if(FC_WP_EventChannel != last_wp_event && enable_injecting) |
326 | if(FC_WP_EventChannel != last_wp_event && enable_injecting) |
327 | { |
327 | { |
328 | ToFlightCtrl.Command = SPI_NCCMD_GPSINFO; |
328 | ToFlightCtrl.Command = SPI_NCCMD_GPSINFO; |
329 | last_wp_event = FC_WP_EventChannel; |
329 | last_wp_event = FC_WP_EventChannel; |
330 | enable_injecting = 0; |
330 | enable_injecting = 0; |
331 | } |
331 | } |
332 | else |
332 | else |
333 | { |
333 | { |
334 | ToFlightCtrl.Command = SPI_CommandSequence[SPI_CommandCounter++]; |
334 | ToFlightCtrl.Command = SPI_CommandSequence[SPI_CommandCounter++]; |
335 | // restart command cycle at the end |
335 | // restart command cycle at the end |
336 | if(SPI_CommandCounter >= sizeof(SPI_CommandSequence)) SPI_CommandCounter = 0; |
336 | if(SPI_CommandCounter >= sizeof(SPI_CommandSequence)) SPI_CommandCounter = 0; |
337 | if(ToFlightCtrl.Command == SPI_NCCMD_KALMAN) enable_injecting = 1; |
337 | if(ToFlightCtrl.Command == SPI_NCCMD_KALMAN) enable_injecting = 1; |
338 | } |
338 | } |
339 | 339 | ||
340 | #define FLAG_GPS_AID 0x01 |
340 | #define FLAG_GPS_AID 0x01 |
341 | switch (ToFlightCtrl.Command) |
341 | switch (ToFlightCtrl.Command) |
342 | { |
342 | { |
343 | case SPI_NCCMD_KALMAN: // wird am häufigsten betätigt |
343 | case SPI_NCCMD_KALMAN: // wird am häufigsten betätigt |
344 | ToFlightCtrl.Param.sByte[0] = (s8) Kalman_K; |
344 | ToFlightCtrl.Param.sByte[0] = (s8) Kalman_K; |
345 | ToFlightCtrl.Param.sByte[1] = (s8) Kalman_MaxFusion; |
345 | ToFlightCtrl.Param.sByte[1] = (s8) Kalman_MaxFusion; |
346 | ToFlightCtrl.Param.sByte[2] = (s8) Kalman_MaxDrift; |
346 | ToFlightCtrl.Param.sByte[2] = (s8) Kalman_MaxDrift; |
347 | ToFlightCtrl.Param.Byte[3] = (u8) Kalman_Kompass; |
347 | ToFlightCtrl.Param.Byte[3] = (u8) Kalman_Kompass; |
348 | ToFlightCtrl.Param.sByte[4] = (s8) ToFcGpsZ; |
348 | ToFlightCtrl.Param.sByte[4] = (s8) ToFcGpsZ; |
349 | ToFlightCtrl.Param.Byte[5] = (s8) ToFC_Rotate_C; |
349 | ToFlightCtrl.Param.Byte[5] = (s8) ToFC_Rotate_C; |
350 | ToFlightCtrl.Param.Byte[6] = (s8) ToFC_Rotate_S; |
350 | ToFlightCtrl.Param.Byte[6] = (s8) ToFC_Rotate_S; |
351 | ToFlightCtrl.Param.Byte[7] = GPS_Aid_StickMultiplikator; |
351 | ToFlightCtrl.Param.Byte[7] = GPS_Aid_StickMultiplikator; |
352 | if(CAM_Orientation.UpdateMask & CAM_UPDATE_AZIMUTH) |
352 | if(CAM_Orientation.UpdateMask & CAM_UPDATE_AZIMUTH) |
353 | { |
353 | { |
354 | ToFlightCtrl.Param.sInt[4] = CAM_Orientation.Azimuth; |
354 | ToFlightCtrl.Param.sInt[4] = CAM_Orientation.Azimuth; |
355 | CAM_Orientation.UpdateMask &= ~CAM_UPDATE_AZIMUTH; |
355 | CAM_Orientation.UpdateMask &= ~CAM_UPDATE_AZIMUTH; |
356 | } |
356 | } |
357 | else |
357 | else |
358 | { |
358 | { |
359 | ToFlightCtrl.Param.sInt[4] = -1; |
359 | ToFlightCtrl.Param.sInt[4] = -1; |
360 | } |
360 | } |
361 | 361 | ||
362 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_NEW_CAMERA_ELEVATION, &tmp)) // Elevation set via 'j' command |
362 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_NEW_CAMERA_ELEVATION, &tmp)) // Elevation set via 'j' command |
363 | { |
363 | { |
364 | POI_KameraNick = tmp; |
364 | POI_KameraNick = tmp; |
365 | } |
365 | } |
366 | else |
366 | else |
367 | { |
367 | { |
368 | //if(FC.StatusFlags2 & FC_STATUS2_CAREFREE) // only, if carefree is active |
368 | //if(FC.StatusFlags2 & FC_STATUS2_CAREFREE) // only, if carefree is active |
369 | POI_KameraNick = CAM_Orientation.Elevation; |
369 | POI_KameraNick = CAM_Orientation.Elevation; |
370 | //else ToFlightCtrl.Param.sInt[5] = 0; |
370 | //else ToFlightCtrl.Param.sInt[5] = 0; |
371 | } |
371 | } |
372 | ToFlightCtrl.Param.sInt[5] = POI_KameraNick; |
372 | ToFlightCtrl.Param.sInt[5] = POI_KameraNick; |
373 | break; |
373 | break; |
374 | 374 | ||
375 | case SPI_NCCMD_VERSION: |
375 | case SPI_NCCMD_VERSION: |
376 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
376 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
377 | //+ higher than the maximum allowed altitude |
377 | //+ higher than the maximum allowed altitude |
378 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
378 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
379 | ToFlightCtrl.Param.Byte[0] = VERSION_MAJOR; |
379 | ToFlightCtrl.Param.Byte[0] = VERSION_MAJOR; |
380 | ToFlightCtrl.Param.Byte[1] = VERSION_MINOR; |
380 | ToFlightCtrl.Param.Byte[1] = VERSION_MINOR; |
381 | ToFlightCtrl.Param.Byte[2] = VERSION_PATCH; |
381 | ToFlightCtrl.Param.Byte[2] = VERSION_PATCH; |
382 | ToFlightCtrl.Param.Byte[3] = FC_SPI_COMPATIBLE; |
382 | ToFlightCtrl.Param.Byte[3] = FC_SPI_COMPATIBLE; |
383 | ToFlightCtrl.Param.Byte[4] = Version_HW; |
383 | ToFlightCtrl.Param.Byte[4] = Version_HW; |
384 | ToFlightCtrl.Param.Byte[5] = DebugOut.StatusGreen; |
384 | ToFlightCtrl.Param.Byte[5] = DebugOut.StatusGreen; |
385 | ToFlightCtrl.Param.Byte[6] = DebugOut.StatusRed; |
385 | ToFlightCtrl.Param.Byte[6] = DebugOut.StatusRed; |
386 | ToFlightCtrl.Param.Byte[7] = ErrorCode; // muss in SPI_NCCMD_VERSION bleiben! (siehe oben) |
386 | ToFlightCtrl.Param.Byte[7] = ErrorCode; // muss in SPI_NCCMD_VERSION bleiben! (siehe oben) |
387 | ToFlightCtrl.Param.Byte[8] = NC_GPS_ModeCharacter; |
387 | ToFlightCtrl.Param.Byte[8] = NC_GPS_ModeCharacter; |
388 | ToFlightCtrl.Param.Byte[9] = SerialLinkOkay; |
388 | ToFlightCtrl.Param.Byte[9] = SerialLinkOkay; |
389 | ToFlightCtrl.Param.Byte[10] = NC_To_FC_Flags; |
389 | ToFlightCtrl.Param.Byte[10] = NC_To_FC_Flags; |
390 | if(AbsoluteFlyingAltitude > 255) ToFlightCtrl.Param.Byte[11] = 0; // then the limitation of the FC doesn't work |
390 | if(AbsoluteFlyingAltitude > 255) ToFlightCtrl.Param.Byte[11] = 0; // then the limitation of the FC doesn't work |
391 | else ToFlightCtrl.Param.Byte[11] = AbsoluteFlyingAltitude; |
391 | else ToFlightCtrl.Param.Byte[11] = AbsoluteFlyingAltitude; |
392 | break; |
392 | break; |
393 | case SPI_MISC: |
393 | case SPI_MISC: |
394 | ToFlightCtrl.Param.Byte[0] = EarthMagneticFieldFiltered/5; |
394 | ToFlightCtrl.Param.Byte[0] = EarthMagneticFieldFiltered/5; |
395 | ToFlightCtrl.Param.Byte[1] = EarthMagneticInclination; |
395 | ToFlightCtrl.Param.Byte[1] = EarthMagneticInclination; |
396 | ToFlightCtrl.Param.Byte[2] = EarthMagneticInclinationTheoretic; |
396 | ToFlightCtrl.Param.Byte[2] = EarthMagneticInclinationTheoretic; |
397 | ToFlightCtrl.Param.Byte[3] = SpeakHoTT; |
397 | ToFlightCtrl.Param.Byte[3] = SpeakHoTT; |
398 | ToFlightCtrl.Param.Byte[4] = NaviData.WaypointIndex; // index of current waypoints running from 0 to WaypointNumber-1 |
398 | ToFlightCtrl.Param.Byte[4] = NaviData.WaypointIndex; // index of current waypoints running from 0 to WaypointNumber-1 |
399 | ToFlightCtrl.Param.Byte[5] = NaviData.WaypointNumber; // number of stored waypoints |
399 | ToFlightCtrl.Param.Byte[5] = NaviData.WaypointNumber; // number of stored waypoints |
400 | ToFlightCtrl.Param.Int[3] = NaviData.TargetPositionDeviation.Distance / 10; |
400 | ToFlightCtrl.Param.Int[3] = NaviData.TargetPositionDeviation.Distance / 10; |
401 | ToFlightCtrl.Param.Byte[8] = NaviData.TargetHoldTime; // time in s to stay at the given target, counts down to 0 if target has been reached |
401 | ToFlightCtrl.Param.Byte[8] = NaviData.TargetHoldTime; // time in s to stay at the given target, counts down to 0 if target has been reached |
402 | ToFlightCtrl.Param.Byte[9] = 0; |
402 | ToFlightCtrl.Param.Byte[9] = 0; |
403 | ToFlightCtrl.Param.Byte[10] = 0; |
403 | ToFlightCtrl.Param.Byte[10] = 0; |
404 | ToFlightCtrl.Param.Byte[11] = 0; |
404 | ToFlightCtrl.Param.Byte[11] = 0; |
405 | SpeakHoTT = 0; |
405 | SpeakHoTT = 0; |
406 | break; |
406 | break; |
407 | 407 | ||
408 | case SPI_NCCMD_GPSINFO: |
408 | case SPI_NCCMD_GPSINFO: |
409 | ToFlightCtrl.Param.Byte[0] = GPSData.Flags; |
409 | ToFlightCtrl.Param.Byte[0] = GPSData.Flags; |
410 | ToFlightCtrl.Param.Byte[1] = GPSData.NumOfSats; |
410 | ToFlightCtrl.Param.Byte[1] = GPSData.NumOfSats; |
411 | ToFlightCtrl.Param.Byte[2] = GPSData.SatFix; |
411 | ToFlightCtrl.Param.Byte[2] = GPSData.SatFix; |
412 | ToFlightCtrl.Param.Byte[3] = GPSData.Speed_Ground / 100; // m/s |
412 | ToFlightCtrl.Param.Byte[3] = GPSData.Speed_Ground / 100; // m/s |
413 | ToFlightCtrl.Param.Int[2] = NaviData.HomePositionDeviation.Distance; // dm //4&5 |
413 | ToFlightCtrl.Param.Int[2] = NaviData.HomePositionDeviation.Distance; // dm //4&5 |
414 | ToFlightCtrl.Param.sInt[3] = NaviData.HomePositionDeviation.Bearing; // deg //6&7 |
414 | ToFlightCtrl.Param.sInt[3] = NaviData.HomePositionDeviation.Bearing; // deg //6&7 |
415 | if(FC_WP_EventChannel > 254) FC_WP_EventChannel = 254; // Muss in SPI_NCCMD_GPSINFO bleiben! (siehe oben) |
415 | if(FC_WP_EventChannel > 254) FC_WP_EventChannel = 254; // Muss in SPI_NCCMD_GPSINFO bleiben! (siehe oben) |
416 | if(FC_WP_EventChannel) LogFC_WP_EventChannel = FC_WP_EventChannel; // to make sure that it will be logged |
416 | if(FC_WP_EventChannel) LogFC_WP_EventChannel = FC_WP_EventChannel; // to make sure that it will be logged |
417 | // ++++++++++++++++++++++++++++++++++ |
417 | // ++++++++++++++++++++++++++++++++++ |
418 | // Waypoint event +++++++++++++++++++ |
418 | // Waypoint event +++++++++++++++++++ |
419 | // ++++++++++++++++++++++++++++++++++ |
419 | // ++++++++++++++++++++++++++++++++++ |
420 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_WP_EVENT_ONCE, &tmp)) |
420 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_WP_EVENT_ONCE, &tmp)) |
421 | { |
421 | { |
422 | ToFlightCtrl.Param.Byte[8] = (s8)(tmp - 127); |
422 | ToFlightCtrl.Param.Byte[8] = (s8)(tmp - 127); |
423 | NCParams_ClearValue(NCPARAMS_WP_EVENT_ONCE); |
423 | NCParams_ClearValue(NCPARAMS_WP_EVENT_ONCE); |
424 | NCParams_ClearValue(NCPARAMS_WP_EVENT_FOREVER); |
424 | NCParams_ClearValue(NCPARAMS_WP_EVENT_FOREVER); |
425 | } |
425 | } |
426 | else |
426 | else |
427 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_WP_EVENT_FOREVER, &tmp)) |
427 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_WP_EVENT_FOREVER, &tmp)) |
428 | { |
428 | { |
429 | ToFlightCtrl.Param.Byte[8] = (s8)(tmp - 127); |
429 | ToFlightCtrl.Param.Byte[8] = (s8)(tmp - 127); |
430 | if(tmp == 0) NCParams_ClearValue(NCPARAMS_WP_EVENT_FOREVER); |
430 | if(tmp == 0) NCParams_ClearValue(NCPARAMS_WP_EVENT_FOREVER); |
431 | } |
431 | } |
432 | else ToFlightCtrl.Param.Byte[8] = (s8)(FC_WP_EventChannel - 127); |
432 | else ToFlightCtrl.Param.Byte[8] = (s8)(FC_WP_EventChannel - 127); |
433 | FC_WP_EventChannel = 0; // the GPS-Routine will set it again |
433 | FC_WP_EventChannel = 0; // the GPS-Routine will set it again |
434 | // ++++++++++++++++++++++++++++++++++ |
434 | // ++++++++++++++++++++++++++++++++++ |
435 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_RATE, &tmp)) |
435 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_RATE, &tmp)) |
436 | { |
436 | { |
437 | ToFlightCtrl.Param.Byte[9] = (u8)tmp; |
437 | ToFlightCtrl.Param.Byte[9] = (u8)tmp; |
438 | } |
438 | } |
439 | else |
439 | else |
440 | { |
440 | { |
441 | ToFlightCtrl.Param.Byte[9] = (u8)ToFC_AltitudeRate; |
441 | ToFlightCtrl.Param.Byte[9] = (u8)ToFC_AltitudeRate; |
442 | } |
442 | } |
443 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_SETPOINT, &tmp)) |
443 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_SETPOINT, &tmp)) |
444 | { |
444 | { |
445 | ToFlightCtrl.Param.sInt[5] = tmp; |
445 | ToFlightCtrl.Param.sInt[5] = tmp; |
446 | } |
446 | } |
447 | else |
447 | else |
448 | { |
448 | { |
449 | ToFlightCtrl.Param.sInt[5] = (s16)ToFC_AltitudeSetpoint; |
449 | ToFlightCtrl.Param.sInt[5] = (s16)ToFC_AltitudeSetpoint; |
450 | } |
450 | } |
451 | break; |
451 | break; |
452 | case SPI_NCCMD_HOTT_INFO: |
452 | case SPI_NCCMD_HOTT_INFO: |
453 | switch(hott_index++) |
453 | switch(hott_index++) |
454 | { |
454 | { |
455 | case 0: |
455 | case 0: |
456 | //Dezimalgrad --> Grad mit Dezimalminuten --> Grad, Minuten, Sekunden |
456 | //Dezimalgrad --> Grad mit Dezimalminuten --> Grad, Minuten, Sekunden |
457 | //53.28 5788 7.4847269 --> N53° 17.14728 E7° 29.08362 --> N53° 17' 8.837" E7° 29' 5.017" |
457 | //53.28 5788 7.4847269 --> N53° 17.14728 E7° 29.08362 --> N53° 17' 8.837" E7° 29' 5.017" |
458 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
458 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
459 | ToFlightCtrl.Param.Byte[0] = 3+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
459 | ToFlightCtrl.Param.Byte[0] = 3+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
460 | ToFlightCtrl.Param.Byte[1] = 9-1; // how many |
460 | ToFlightCtrl.Param.Byte[1] = 9-1; // how many |
461 | //----------------------------- |
461 | //----------------------------- |
462 | ToFlightCtrl.Param.Byte[2] = GyroCompassCorrected / 20;//NaviData.HomePositionDeviation.Bearing / 2; |
462 | ToFlightCtrl.Param.Byte[2] = GyroCompassCorrected / 20;//NaviData.HomePositionDeviation.Bearing / 2; |
463 | i1 = GPSData.Speed_Ground; // in cm/sec |
463 | i1 = GPSData.Speed_Ground; // in cm/sec |
464 | i1 *= 36; |
464 | i1 *= 36; |
465 | i1 /= 1000; |
465 | i1 /= 1000; |
466 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
466 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
467 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
467 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
468 | //----------------------------- |
468 | //----------------------------- |
469 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 1; // 1 = S |
469 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 1; // 1 = S |
470 | else ToFlightCtrl.Param.Byte[5] = 0; // 1 = S |
470 | else ToFlightCtrl.Param.Byte[5] = 0; // 1 = S |
471 | i1 = abs(GPSData.Position.Latitude)/10000000L; |
471 | i1 = abs(GPSData.Position.Latitude)/10000000L; |
472 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
472 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
473 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
473 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
474 | i1 *= 100; |
474 | i1 *= 100; |
475 | // Minuten |
475 | // Minuten |
476 | i2 *= 6; |
476 | i2 *= 6; |
477 | i2 /= 10; |
477 | i2 /= 10; |
478 | i1 += i2 / 100000; |
478 | i1 += i2 / 100000; |
479 | i2 = i2 % 100000; |
479 | i2 = i2 % 100000; |
480 | i2 /= 10; |
480 | i2 /= 10; |
481 | ToFlightCtrl.Param.Byte[6] = i1 % 256; |
481 | ToFlightCtrl.Param.Byte[6] = i1 % 256; |
482 | ToFlightCtrl.Param.Byte[7] = i1 / 256; |
482 | ToFlightCtrl.Param.Byte[7] = i1 / 256; |
483 | ToFlightCtrl.Param.Byte[8] = i2 % 256; |
483 | ToFlightCtrl.Param.Byte[8] = i2 % 256; |
484 | ToFlightCtrl.Param.Byte[9] = i2 / 256; |
484 | ToFlightCtrl.Param.Byte[9] = i2 / 256; |
485 | break; |
485 | break; |
486 | case 1: |
486 | case 1: |
487 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
487 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
488 | ToFlightCtrl.Param.Byte[0] = 11+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
488 | ToFlightCtrl.Param.Byte[0] = 11+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
489 | ToFlightCtrl.Param.Byte[1] = 8-1; // how many |
489 | ToFlightCtrl.Param.Byte[1] = 8-1; // how many |
490 | //----------------------------- |
490 | //----------------------------- |
491 | if(GPSData.Position.Longitude < 0) ToFlightCtrl.Param.Byte[2] = 1; // 1 = E |
491 | if(GPSData.Position.Longitude < 0) ToFlightCtrl.Param.Byte[2] = 1; // 1 = E |
492 | else ToFlightCtrl.Param.Byte[2] = 0; // 1 = S |
492 | else ToFlightCtrl.Param.Byte[2] = 0; // 1 = S |
493 | i1 = abs(GPSData.Position.Longitude)/10000000L; |
493 | i1 = abs(GPSData.Position.Longitude)/10000000L; |
494 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
494 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
495 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
495 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
496 | i1 *= 100; |
496 | i1 *= 100; |
497 | // Minuten |
497 | // Minuten |
498 | i2 *= 6; |
498 | i2 *= 6; |
499 | i2 /= 10; |
499 | i2 /= 10; |
500 | i1 += i2 / 100000; |
500 | i1 += i2 / 100000; |
501 | i2 = i2 % 100000; |
501 | i2 = i2 % 100000; |
502 | i2 /= 10; |
502 | i2 /= 10; |
503 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
503 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
504 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
504 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
505 | ToFlightCtrl.Param.Byte[5] = i2 % 256; |
505 | ToFlightCtrl.Param.Byte[5] = i2 % 256; |
506 | ToFlightCtrl.Param.Byte[6] = i2 / 256; |
506 | ToFlightCtrl.Param.Byte[6] = i2 / 256; |
507 | //----------------------------- |
507 | //----------------------------- |
508 | i1 = NaviData.HomePositionDeviation.Distance / 10; // dann in m |
508 | i1 = NaviData.HomePositionDeviation.Distance / 10; // dann in m |
509 | ToFlightCtrl.Param.Byte[7] = i1 % 256; |
509 | ToFlightCtrl.Param.Byte[7] = i1 % 256; |
510 | ToFlightCtrl.Param.Byte[8] = i1 / 256; |
510 | ToFlightCtrl.Param.Byte[8] = i1 / 256; |
511 | break; |
511 | break; |
512 | case 2: |
512 | case 2: |
513 | ToFlightCtrl.Param.Byte[11] = HOTT_GENERAL_PACKET_ID; |
513 | ToFlightCtrl.Param.Byte[11] = HOTT_GENERAL_PACKET_ID; |
514 | ToFlightCtrl.Param.Byte[0] = 5+3; // index // +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
514 | ToFlightCtrl.Param.Byte[0] = 5+3; // index // +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
515 | ToFlightCtrl.Param.Byte[1] = 2; // how many |
515 | ToFlightCtrl.Param.Byte[1] = 2; // how many |
516 | ToFlightCtrl.Param.Byte[2] = EarthMagneticField / (5 * 2); |
516 | ToFlightCtrl.Param.Byte[2] = EarthMagneticField / (5 * 2); |
517 | ToFlightCtrl.Param.Byte[3] = EarthMagneticInclination / 2; |
517 | ToFlightCtrl.Param.Byte[3] = EarthMagneticInclination / 2; |
518 | break; |
518 | break; |
519 | case 3: |
519 | case 3: |
520 | ToFlightCtrl.Param.Byte[11] = JETI_GPS_PACKET_ID1; |
520 | ToFlightCtrl.Param.Byte[11] = JETI_GPS_PACKET_ID1; |
521 | ToFlightCtrl.Param.Byte[0] = 0; // index |
521 | ToFlightCtrl.Param.Byte[0] = 0; // index |
522 | ToFlightCtrl.Param.Byte[1] = 4; // how many |
522 | ToFlightCtrl.Param.Byte[1] = 4; // how many |
523 | //JetiExData[14].Value = 53 * 0x10000 + 23467; |
523 | //JetiExData[14].Value = 53 * 0x10000 + 23467; |
524 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 0x40; |
524 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 0x40; |
525 | else ToFlightCtrl.Param.Byte[5] = 0x00; |
525 | else ToFlightCtrl.Param.Byte[5] = 0x00; |
526 | ToFlightCtrl.Param.Byte[4] = abs(GPSData.Position.Latitude)/10000000L; |
526 | ToFlightCtrl.Param.Byte[4] = abs(GPSData.Position.Latitude)/10000000L; |
527 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
527 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
528 | i2 *= 6; |
528 | i2 *= 6; |
529 | i2 /= 1000; |
529 | i2 /= 1000; |
530 | ToFlightCtrl.Param.Byte[3] = i2 / 256; |
530 | ToFlightCtrl.Param.Byte[3] = i2 / 256; |
531 | ToFlightCtrl.Param.Byte[2] = i2 % 256; |
531 | ToFlightCtrl.Param.Byte[2] = i2 % 256; |
532 | break; |
532 | break; |
533 | case 4: |
533 | case 4: |
534 | ToFlightCtrl.Param.Byte[11] = JETI_GPS_PACKET_ID2; |
534 | ToFlightCtrl.Param.Byte[11] = JETI_GPS_PACKET_ID2; |
535 | ToFlightCtrl.Param.Byte[0] = 0; // index |
535 | ToFlightCtrl.Param.Byte[0] = 0; // index |
536 | ToFlightCtrl.Param.Byte[1] = 4; // how many |
536 | ToFlightCtrl.Param.Byte[1] = 4; // how many |
537 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 0x60; |
537 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 0x60; |
538 | else ToFlightCtrl.Param.Byte[5] = 0x20; |
538 | else ToFlightCtrl.Param.Byte[5] = 0x20; |
539 | ToFlightCtrl.Param.Byte[4] = abs(GPSData.Position.Longitude)/10000000L; |
539 | ToFlightCtrl.Param.Byte[4] = abs(GPSData.Position.Longitude)/10000000L; |
540 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
540 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
541 | i2 *= 6; |
541 | i2 *= 6; |
542 | i2 /= 1000; |
542 | i2 /= 1000; |
543 | ToFlightCtrl.Param.Byte[3] = i2 / 256; |
543 | ToFlightCtrl.Param.Byte[3] = i2 / 256; |
544 | ToFlightCtrl.Param.Byte[2] = i2 % 256; |
544 | ToFlightCtrl.Param.Byte[2] = i2 % 256; |
545 | hott_index = 0; |
545 | hott_index = 0; |
546 | break; |
546 | break; |
547 | default: |
547 | default: |
548 | ToFlightCtrl.Param.Byte[0] = 255; |
548 | ToFlightCtrl.Param.Byte[0] = 255; |
549 | hott_index = 0; |
549 | hott_index = 0; |
550 | break; |
550 | break; |
551 | } |
551 | } |
552 | break; |
552 | break; |
553 | default: |
553 | default: |
554 | break; |
554 | break; |
555 | // 0 = 0,1 |
555 | // 0 = 0,1 |
556 | // 1 = 2,3 |
556 | // 1 = 2,3 |
557 | // 2 = 4,5 |
557 | // 2 = 4,5 |
558 | // 3 = 6,7 |
558 | // 3 = 6,7 |
559 | // 4 = 8,9 |
559 | // 4 = 8,9 |
560 | // 5 = 10,11 |
560 | // 5 = 10,11 |
561 | } |
561 | } |
562 | VIC_ITCmd(SSP0_ITLine, ENABLE); // enable SPI interrupt |
562 | VIC_ITCmd(SSP0_ITLine, ENABLE); // enable SPI interrupt |
563 | switch(FromFlightCtrl.Command) |
563 | switch(FromFlightCtrl.Command) |
564 | { |
564 | { |
565 | case SPI_FCCMD_USER: |
565 | case SPI_FCCMD_USER: |
566 | Parameter.User1 = FromFlightCtrl.Param.Byte[0]; |
566 | Parameter.User1 = FromFlightCtrl.Param.Byte[0]; |
567 | Parameter.User2 = FromFlightCtrl.Param.Byte[1]; |
567 | Parameter.User2 = FromFlightCtrl.Param.Byte[1]; |
568 | Parameter.User3 = FromFlightCtrl.Param.Byte[2]; |
568 | Parameter.User3 = FromFlightCtrl.Param.Byte[2]; |
569 | Parameter.User4 = FromFlightCtrl.Param.Byte[3]; |
569 | Parameter.User4 = FromFlightCtrl.Param.Byte[3]; |
570 | Parameter.User5 = FromFlightCtrl.Param.Byte[4]; |
570 | Parameter.User5 = FromFlightCtrl.Param.Byte[4]; |
571 | Parameter.User6 = FromFlightCtrl.Param.Byte[5]; |
571 | Parameter.User6 = FromFlightCtrl.Param.Byte[5]; |
572 | Parameter.User7 = FromFlightCtrl.Param.Byte[6]; |
572 | Parameter.User7 = FromFlightCtrl.Param.Byte[6]; |
573 | Parameter.User8 = FromFlightCtrl.Param.Byte[7]; |
573 | Parameter.User8 = FromFlightCtrl.Param.Byte[7]; |
574 | if(ClearFCStatusFlags) |
574 | if(ClearFCStatusFlags) |
575 | { |
575 | { |
576 | FC.StatusFlags = 0; |
576 | FC.StatusFlags = 0; |
577 | ClearFCStatusFlags = 0; |
577 | ClearFCStatusFlags = 0; |
578 | } |
578 | } |
579 | FC.StatusFlags |= FromFlightCtrl.Param.Byte[8]; |
579 | FC.StatusFlags |= FromFlightCtrl.Param.Byte[8]; |
580 | if(FC.StatusFlags & FC_STATUS_CALIBRATE && !FCCalibActive) |
580 | if(FC.StatusFlags & FC_STATUS_CALIBRATE && !FCCalibActive) |
581 | { |
581 | { |
582 | HeadFreeStartAngle = (3600 + Compass_Heading * 10 - GeoMagDec) % 3600; |
582 | HeadFreeStartAngle = (3600 + Compass_Heading * 10 - GeoMagDec) % 3600; |
583 | Compass_Init(); |
583 | Compass_Init(); |
584 | FCCalibActive = 10; |
584 | FCCalibActive = 10; |
585 | FC_is_Calibrated = 0; |
585 | FC_is_Calibrated = 0; |
586 | } |
586 | } |
587 | else |
587 | else |
588 | { |
588 | { |
589 | if(FCCalibActive) |
589 | if(FCCalibActive) |
590 | { |
590 | { |
591 | if(--FCCalibActive == 0) |
591 | if(--FCCalibActive == 0) |
592 | { |
592 | { |
593 | FC_is_Calibrated = 1; |
593 | FC_is_Calibrated = 1; |
594 | ExtCompassOrientation = GetExtCompassOrientation(); |
594 | ExtCompassOrientation = GetExtCompassOrientation(); |
595 | if(ExtCompassOrientation != Calibration.Version / 16) NCMAG_IsCalibrated = 0; |
595 | if(ExtCompassOrientation != Calibration.Version / 16) NCMAG_IsCalibrated = 0; |
596 | } |
596 | } |
597 | } |
597 | } |
598 | } |
598 | } |
599 | if(FC.StatusFlags & FC_STATUS_START) |
599 | if(FC.StatusFlags & FC_STATUS_START) |
600 | { |
600 | { |
601 | if(Compass_Heading != -1) HeadFreeStartAngle = (3600 + Compass_Heading * 10 - GeoMagDec) % 3600; else |
601 | if(Compass_Heading != -1) HeadFreeStartAngle = (3600 + Compass_Heading * 10 - GeoMagDec) % 3600; else |
602 | HeadFreeStartAngle = GyroCompassCorrected; |
602 | HeadFreeStartAngle = GyroCompassCorrected; |
603 | } |
603 | } |
604 | 604 | ||
605 | if((Parameter.ExtraConfig & CFG_TEACHABLE_CAREFREE)) |
605 | if((Parameter.ExtraConfig & CFG_TEACHABLE_CAREFREE)) |
606 | { |
606 | { |
607 | if(!(FC.StatusFlags2 & FC_STATUS2_CAREFREE)) // CF ist jetzt ausgeschaltet -> neue Richtung lernen |
607 | if(!(FC.StatusFlags2 & FC_STATUS2_CAREFREE)) // CF ist jetzt ausgeschaltet -> neue Richtung lernen |
608 | { |
608 | { |
609 | if((NaviData.HomePositionDeviation.Distance > 200) && (NCFlags & NC_FLAG_GPS_OK)) // nur bei ausreichender Distance -> 20m |
609 | if((NaviData.HomePositionDeviation.Distance > 200) && (NCFlags & NC_FLAG_GPS_OK)) // nur bei ausreichender Distance -> 20m |
610 | { |
610 | { |
611 | HeadFreeStartAngle = (10 * NaviData.HomePositionDeviation.Bearing + 1800 + 3600 - Parameter.OrientationAngle * 150) % 3600; // in 0.1° |
611 | HeadFreeStartAngle = (10 * NaviData.HomePositionDeviation.Bearing + 1800 + 3600 - Parameter.OrientationAngle * 150) % 3600; // in 0.1° |
612 | } |
612 | } |
613 | else // Ansonsten die aktuelle Richtung übernehmen |
613 | else // Ansonsten die aktuelle Richtung übernehmen |
614 | HeadFreeStartAngle = GyroCompassCorrected; // in 0.1° |
614 | HeadFreeStartAngle = GyroCompassCorrected; // in 0.1° |
615 | } |
615 | } |
616 | } |
616 | } |
617 | Parameter.ActiveSetting = FromFlightCtrl.Param.Byte[9]; |
617 | Parameter.ActiveSetting = FromFlightCtrl.Param.Byte[9]; |
618 | FC.BAT_Voltage = FromFlightCtrl.Param.Byte[10]; |
618 | FC.BAT_Voltage = FromFlightCtrl.Param.Byte[10]; |
619 | DebugOut.Analog[7] = FC.BAT_Voltage; |
619 | DebugOut.Analog[7] = FC.BAT_Voltage; |
620 | DebugOut.Analog[5] = FC.StatusFlags; |
620 | DebugOut.Analog[5] = FC.StatusFlags; |
621 | NaviData.FCStatusFlags = FC.StatusFlags; |
621 | NaviData.FCStatusFlags = FC.StatusFlags; |
622 | if(FC.StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) NaviData.FCStatusFlags &= ~FC_STATUS_FLY; |
622 | if(FC.StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) NaviData.FCStatusFlags &= ~FC_STATUS_FLY; |
623 | FC.StatusFlags2 = FromFlightCtrl.Param.Byte[11]; |
623 | FC.StatusFlags2 = FromFlightCtrl.Param.Byte[11]; |
624 | NaviData.FCStatusFlags2 = (NaviData.FCStatusFlags2 & (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE)) | (FC.StatusFlags2 & (0xff - (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE))); |
624 | NaviData.FCStatusFlags2 = (NaviData.FCStatusFlags2 & (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE)) | (FC.StatusFlags2 & (0xff - (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE))); |
625 | 625 | ||
626 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT1_ACTIVE; |
626 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT1_ACTIVE; |
627 | else |
627 | else |
628 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT1_ACTIVE; |
628 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT1_ACTIVE; |
629 | 629 | ||
630 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT2_ACTIVE; |
630 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT2_ACTIVE; |
631 | else |
631 | else |
632 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT2_ACTIVE; |
632 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT2_ACTIVE; |
633 | 633 | ||
634 | Logging_FCStatusFlags1 |= FC.StatusFlags; |
634 | Logging_FCStatusFlags1 |= FC.StatusFlags; |
635 | Logging_FCStatusFlags2 |= FC.StatusFlags2; |
635 | Logging_FCStatusFlags2 |= FC.StatusFlags2; |
636 | break; |
636 | break; |
637 | 637 | ||
638 | case SPI_FCCMD_BL_ACCU: |
638 | case SPI_FCCMD_BL_ACCU: |
639 | FC.BAT_Current = FromFlightCtrl.Param.Int[0]; |
639 | FC.BAT_Current = FromFlightCtrl.Param.Int[0]; |
640 | DebugOut.Analog[8] = FC.BAT_Current; |
640 | DebugOut.Analog[8] = FC.BAT_Current; |
641 | FC.BAT_UsedCapacity = FromFlightCtrl.Param.Int[1]; |
641 | FC.BAT_UsedCapacity = FromFlightCtrl.Param.Int[1]; |
642 | Parameter.NaviGpsModeControl = FromFlightCtrl.Param.Byte[4]; |
642 | Parameter.NaviGpsModeControl = FromFlightCtrl.Param.Byte[4]; |
643 | FromFC_VarioCharacter = FromFlightCtrl.Param.Byte[5]; |
643 | FromFC_VarioCharacter = FromFlightCtrl.Param.Byte[5]; |
644 | Motor_Version[FromFlightCtrl.Param.Byte[6]] = FromFlightCtrl.Param.Byte[7]; |
644 | Motor_Version[FromFlightCtrl.Param.Byte[6]] = FromFlightCtrl.Param.Byte[7]; |
645 | Motor[FromFlightCtrl.Param.Byte[6]].MaxPWM = FromFlightCtrl.Param.Byte[8]; |
645 | Motor[FromFlightCtrl.Param.Byte[6]].MaxPWM = FromFlightCtrl.Param.Byte[8]; |
646 | Motor[FromFlightCtrl.Param.Byte[6]].State = FromFlightCtrl.Param.Byte[9]; |
646 | Motor[FromFlightCtrl.Param.Byte[6]].State = FromFlightCtrl.Param.Byte[9]; |
647 | Motor[FromFlightCtrl.Param.Byte[6]].Temperature = FromFlightCtrl.Param.Byte[10]; |
647 | Motor[FromFlightCtrl.Param.Byte[6]].Temperature = FromFlightCtrl.Param.Byte[10]; |
648 | Motor[FromFlightCtrl.Param.Byte[6]].Current = FromFlightCtrl.Param.Byte[11]; |
648 | Motor[FromFlightCtrl.Param.Byte[6]].Current = FromFlightCtrl.Param.Byte[11]; |
649 | if(FromFC_VarioCharacter == '+' || FromFC_VarioCharacter == '-') // manual setpoint clears the NC-Parameter command |
649 | if(FromFC_VarioCharacter == '+' || FromFC_VarioCharacter == '-') // manual setpoint clears the NC-Parameter command |
650 | { |
650 | { |
651 | NCParams_ClearValue(NCPARAMS_ALTITUDE_RATE); |
651 | NCParams_ClearValue(NCPARAMS_ALTITUDE_RATE); |
652 | } |
652 | } |
653 | NaviData.UBat = FC.BAT_Voltage; |
653 | NaviData.UBat = FC.BAT_Voltage; |
654 | NaviData.Current = FC.BAT_Current; |
654 | NaviData.Current = FC.BAT_Current; |
655 | NaviData.UsedCapacity = FC.BAT_UsedCapacity; |
655 | NaviData.UsedCapacity = FC.BAT_UsedCapacity; |
656 | break; |
656 | break; |
657 | case SPI_FCCMD_PARAMETER1: |
657 | case SPI_FCCMD_PARAMETER1: |
658 | Parameter.LowVoltageWarning = FromFlightCtrl.Param.Byte[0]; |
658 | Parameter.LowVoltageWarning = FromFlightCtrl.Param.Byte[0]; |
659 | CHK_POTI_MM(Parameter.NaviGpsGain,FromFlightCtrl.Param.Byte[1],0,255); |
659 | CHK_POTI_MM(Parameter.NaviGpsGain,FromFlightCtrl.Param.Byte[1],0,255); |
660 | CHK_POTI_MM(Parameter.NaviGpsP,FromFlightCtrl.Param.Byte[2],0,255); |
660 | CHK_POTI_MM(Parameter.NaviGpsP,FromFlightCtrl.Param.Byte[2],0,255); |
661 | CHK_POTI_MM(Parameter.NaviGpsI,FromFlightCtrl.Param.Byte[3],0,255); |
661 | CHK_POTI_MM(Parameter.NaviGpsI,FromFlightCtrl.Param.Byte[3],0,255); |
662 | CHK_POTI_MM(Parameter.NaviGpsD,FromFlightCtrl.Param.Byte[4],0,255); |
662 | CHK_POTI_MM(Parameter.NaviGpsD,FromFlightCtrl.Param.Byte[4],0,255); |
663 | CHK_POTI_MM(Parameter.NaviGpsACC,FromFlightCtrl.Param.Byte[5],0,255); |
663 | CHK_POTI_MM(Parameter.NaviGpsACC,FromFlightCtrl.Param.Byte[5],0,255); |
664 | Parameter.NaviGpsMinSat = FromFlightCtrl.Param.Byte[6]; |
664 | Parameter.NaviGpsMinSat = FromFlightCtrl.Param.Byte[6]; |
665 | Parameter.NaviStickThreshold = FromFlightCtrl.Param.Byte[7]; |
665 | Parameter.NaviStickThreshold = FromFlightCtrl.Param.Byte[7]; |
666 | CHK_POTI_MM(Parameter.NaviOperatingRadius,FromFlightCtrl.Param.Byte[8],0,255); |
666 | CHK_POTI_MM(Parameter.NaviOperatingRadius,FromFlightCtrl.Param.Byte[8],0,255); |
667 | CHK_POTI_MM(Parameter.NaviWindCorrection,FromFlightCtrl.Param.Byte[9],0,255); |
667 | CHK_POTI_MM(Parameter.NaviWindCorrection,FromFlightCtrl.Param.Byte[9],0,255); |
668 | CHK_POTI_MM(Parameter.NaviAccCompensation,FromFlightCtrl.Param.Byte[10],0,255); |
668 | CHK_POTI_MM(Parameter.NaviAccCompensation,FromFlightCtrl.Param.Byte[10],0,255); |
669 | CHK_POTI_MM(Parameter.NaviAngleLimitation,FromFlightCtrl.Param.Byte[11],0,255); |
669 | CHK_POTI_MM(Parameter.NaviAngleLimitation,FromFlightCtrl.Param.Byte[11],0,255); |
670 | break; |
670 | break; |
671 | case SPI_FCCMD_PARAMETER2: |
671 | case SPI_FCCMD_PARAMETER2: |
672 | CHK_POTI_MM(Parameter.NaviOut1Parameter,FromFlightCtrl.Param.Byte[0],0,255); |
672 | CHK_POTI_MM(Parameter.NaviOut1Parameter,FromFlightCtrl.Param.Byte[0],0,255); |
673 | if(FromFlightCtrl.Param.Byte[1]) FC.FromFC_SpeakHoTT = FromFlightCtrl.Param.Byte[1]; // will be cleared in the SD-Logging |
673 | if(FromFlightCtrl.Param.Byte[1]) FC.FromFC_SpeakHoTT = FromFlightCtrl.Param.Byte[1]; // will be cleared in the SD-Logging |
674 | Parameter.FromFC_LandingSpeed = FromFlightCtrl.Param.Byte[2]; |
674 | Parameter.FromFC_LandingSpeed = FromFlightCtrl.Param.Byte[2]; |
675 | Parameter.ComingHomeAltitude = FromFlightCtrl.Param.Byte[3]; |
675 | Parameter.ComingHomeAltitude = FromFlightCtrl.Param.Byte[3]; |
676 | break; |
676 | break; |
677 | case SPI_FCCMD_STICK: |
677 | case SPI_FCCMD_STICK: |
678 | FC.StickGas = FromFlightCtrl.Param.sByte[0]; |
678 | FC.StickGas = FromFlightCtrl.Param.sByte[0]; |
679 | FC.StickYaw = FromFlightCtrl.Param.sByte[1]; |
679 | FC.StickYaw = FromFlightCtrl.Param.sByte[1]; |
680 | FC.StickRoll = FromFlightCtrl.Param.sByte[2]; |
680 | FC.StickRoll = FromFlightCtrl.Param.sByte[2]; |
681 | FC.StickNick = FromFlightCtrl.Param.sByte[3]; |
681 | FC.StickNick = FromFlightCtrl.Param.sByte[3]; |
682 | FC.Poti[0] = FromFlightCtrl.Param.Byte[4]; |
682 | FC.Poti[0] = FromFlightCtrl.Param.Byte[4]; |
683 | FC.Poti[1] = FromFlightCtrl.Param.Byte[5]; |
683 | FC.Poti[1] = FromFlightCtrl.Param.Byte[5]; |
684 | FC.Poti[2] = FromFlightCtrl.Param.Byte[6]; |
684 | FC.Poti[2] = FromFlightCtrl.Param.Byte[6]; |
685 | FC.Poti[3] = FromFlightCtrl.Param.Byte[7]; |
685 | FC.Poti[3] = FromFlightCtrl.Param.Byte[7]; |
686 | FC.Poti[4] = FromFlightCtrl.Param.Byte[8]; |
686 | FC.Poti[4] = FromFlightCtrl.Param.Byte[8]; |
687 | FC.Poti[5] = FromFlightCtrl.Param.Byte[9]; |
687 | FC.Poti[5] = FromFlightCtrl.Param.Byte[9]; |
688 | FC.Poti[6] = FromFlightCtrl.Param.Byte[10]; |
688 | FC.Poti[6] = FromFlightCtrl.Param.Byte[10]; |
689 | FC.Poti[7] = FromFlightCtrl.Param.Byte[11]; |
689 | FC.Poti[7] = FromFlightCtrl.Param.Byte[11]; |
690 | CHK_POTI_MM(WaypointAcceleration,WaypointAccelerationSetting,0,255); // that could be a Poti-Value |
690 | CHK_POTI_MM(WaypointAcceleration,WaypointAccelerationSetting,0,255); // that could be a Poti-Value |
691 | break; |
691 | break; |
692 | 692 | ||
693 | case SPI_FCCMD_MISC: |
693 | case SPI_FCCMD_MISC: |
694 | if(CompassCalState != FromFlightCtrl.Param.Byte[0]) |
694 | if(CompassCalState != FromFlightCtrl.Param.Byte[0]) |
695 | { // put only new CompassCalState into queue to send via I2C |
695 | { // put only new CompassCalState into queue to send via I2C |
696 | // if(FromFlightCtrl.Param.Byte[0] == CompassCalState+1 || FromFlightCtrl.Param.Byte[0] == 0) |
696 | // if(FromFlightCtrl.Param.Byte[0] == CompassCalState+1 || FromFlightCtrl.Param.Byte[0] == 0) |
697 | { |
697 | { |
698 | CompassCalState = FromFlightCtrl.Param.Byte[0]; |
698 | CompassCalState = FromFlightCtrl.Param.Byte[0]; |
699 | Compass_SetCalState(CompassCalState); |
699 | Compass_SetCalState(CompassCalState); |
700 | } |
700 | } |
701 | // else CompassCalState = 0; |
701 | // else CompassCalState = 0; |
702 | } |
702 | } |
703 | Parameter.NaviPH_LoginTime = FromFlightCtrl.Param.Byte[1]; |
703 | Parameter.NaviPH_LoginTime = FromFlightCtrl.Param.Byte[1]; |
704 | NaviData.Variometer = (NaviData.Variometer + 2 * (FromFlightCtrl.Param.sInt[1] - NaviData.Altimeter)) / 2; // provisorisch |
704 | NaviData.Variometer = (NaviData.Variometer + 2 * (FromFlightCtrl.Param.sInt[1] - NaviData.Altimeter)) / 2; // provisorisch |
705 | NaviData.Altimeter = FromFlightCtrl.Param.sInt[1]; // in 5cm |
705 | NaviData.Altimeter = FromFlightCtrl.Param.sInt[1]; // in 5cm |
706 | NaviData.SetpointAltitude = FromFlightCtrl.Param.sInt[2]; // in 5cm |
706 | NaviData.SetpointAltitude = FromFlightCtrl.Param.sInt[2]; // in 5cm |
707 | CHK_POTI_MM(Parameter.NaviGpsPLimit,FromFlightCtrl.Param.Byte[6],0,255); |
707 | CHK_POTI_MM(Parameter.NaviGpsPLimit,FromFlightCtrl.Param.Byte[6],0,255); |
708 | CHK_POTI_MM(Parameter.NaviGpsILimit,FromFlightCtrl.Param.Byte[7],0,255); |
708 | CHK_POTI_MM(Parameter.NaviGpsILimit,FromFlightCtrl.Param.Byte[7],0,255); |
709 | CHK_POTI_MM(Parameter.NaviGpsDLimit,FromFlightCtrl.Param.Byte[8],0,255); |
709 | CHK_POTI_MM(Parameter.NaviGpsDLimit,FromFlightCtrl.Param.Byte[8],0,255); |
710 | FC.RC_Quality = FromFlightCtrl.Param.Byte[9]; |
710 | FC.RC_Quality = FromFlightCtrl.Param.Byte[9]; |
711 | NaviData.RC_Quality = FC.RC_Quality; |
711 | NaviData.RC_Quality = FC.RC_Quality; |
712 | NC_Wait_for_LED = FromFlightCtrl.Param.Byte[10]; |
712 | NC_Wait_for_LED = FromFlightCtrl.Param.Byte[10]; |
713 | // FC.RC_RSSI = FromFlightCtrl.Param.Byte[10]; |
713 | // FC.RC_RSSI = FromFlightCtrl.Param.Byte[10]; |
714 | // if(!FC.RC_RSSI) NaviData.RC_Quality = FC.RC_Quality; else NaviData.RC_Quality = FC.RC_RSSI; |
714 | // if(!FC.RC_RSSI) NaviData.RC_Quality = FC.RC_Quality; else NaviData.RC_Quality = FC.RC_RSSI; |
715 | // NaviData.RC_RSSI = FC.RC_RSSI; |
715 | // NaviData.RC_RSSI = FC.RC_RSSI; |
716 | NaviData.Gas = (FC.BAT_Voltage * (u32) FromFlightCtrl.Param.Byte[11]) / (u32) Parameter.LowVoltageWarning; |
716 | NaviData.Gas = (FC.BAT_Voltage * (u32) FromFlightCtrl.Param.Byte[11]) / (u32) Parameter.LowVoltageWarning; |
717 | break; |
717 | break; |
718 | 718 | ||
719 | case SPI_FCCMD_SERVOS: |
719 | case SPI_FCCMD_SERVOS: |
720 | ServoParams.Refresh = FromFlightCtrl.Param.Byte[0]; |
720 | ServoParams.Refresh = FromFlightCtrl.Param.Byte[0]; |
721 | ServoParams.CompInvert = FromFlightCtrl.Param.Byte[1]; |
721 | ServoParams.CompInvert = FromFlightCtrl.Param.Byte[1]; |
722 | ServoParams.NickControl = FromFlightCtrl.Param.Byte[2]; |
722 | ServoParams.NickControl = FromFlightCtrl.Param.Byte[2]; |
723 | ServoParams.NickComp = FromFlightCtrl.Param.Byte[3]; |
723 | ServoParams.NickComp = FromFlightCtrl.Param.Byte[3]; |
724 | ServoParams.NickMin = FromFlightCtrl.Param.Byte[4]; |
724 | ServoParams.NickMin = FromFlightCtrl.Param.Byte[4]; |
725 | ServoParams.NickMax = FromFlightCtrl.Param.Byte[5]; |
725 | ServoParams.NickMax = FromFlightCtrl.Param.Byte[5]; |
726 | ServoParams.RollControl = FromFlightCtrl.Param.Byte[6]; |
726 | ServoParams.RollControl = FromFlightCtrl.Param.Byte[6]; |
727 | ServoParams.RollComp = FromFlightCtrl.Param.Byte[7]; |
727 | ServoParams.RollComp = FromFlightCtrl.Param.Byte[7]; |
728 | ServoParams.RollMin = FromFlightCtrl.Param.Byte[8]; |
728 | ServoParams.RollMin = FromFlightCtrl.Param.Byte[8]; |
729 | ServoParams.RollMax = FromFlightCtrl.Param.Byte[9]; |
729 | ServoParams.RollMax = FromFlightCtrl.Param.Byte[9]; |
730 | BL_MinOfMaxPWM = FromFlightCtrl.Param.Byte[10]; |
730 | BL_MinOfMaxPWM = FromFlightCtrl.Param.Byte[10]; |
731 | FC_I2C_ErrorConter = FromFlightCtrl.Param.Byte[11]; |
731 | FC_I2C_ErrorConter = FromFlightCtrl.Param.Byte[11]; |
732 | break; |
732 | break; |
733 | 733 | ||
734 | case SPI_FCCMD_VERSION: |
734 | case SPI_FCCMD_VERSION: |
735 | FC_Version.Major = FromFlightCtrl.Param.Byte[0]; |
735 | FC_Version.Major = FromFlightCtrl.Param.Byte[0]; |
736 | FC_Version.Minor = FromFlightCtrl.Param.Byte[1]; |
736 | FC_Version.Minor = FromFlightCtrl.Param.Byte[1]; |
737 | FC_Version.Patch = FromFlightCtrl.Param.Byte[2]; |
737 | FC_Version.Patch = FromFlightCtrl.Param.Byte[2]; |
738 | FC_Version.Compatible = FromFlightCtrl.Param.Byte[3]; |
738 | FC_Version.Compatible = FromFlightCtrl.Param.Byte[3]; |
739 | FC_Version.Hardware = FromFlightCtrl.Param.Byte[4]; |
739 | FC_Version.Hardware = FromFlightCtrl.Param.Byte[4]; |
740 | FC.Error[0] |= FromFlightCtrl.Param.Byte[5]; |
740 | FC.Error[0] |= FromFlightCtrl.Param.Byte[5]; |
741 | FC.Error[1] |= FromFlightCtrl.Param.Byte[6]; |
741 | FC.Error[1] |= FromFlightCtrl.Param.Byte[6]; |
742 | if(FromFlightCtrl.Param.Byte[7] >= 68 && FromFlightCtrl.Param.Byte[7] <= 188) |
742 | if(FromFlightCtrl.Param.Byte[7] >= 68 && FromFlightCtrl.Param.Byte[7] <= 188) |
743 | { |
743 | { |
744 | FC.FromFC_DisableDeclination = 1; |
744 | FC.FromFC_DisableDeclination = 1; |
745 | FC.FromFC_CompassOffset = 10 * (signed char) ((unsigned char) FromFlightCtrl.Param.Byte[7] - 128); |
745 | FC.FromFC_CompassOffset = 10 * (signed char) ((unsigned char) FromFlightCtrl.Param.Byte[7] - 128); |
746 | GeoMagDec = 0; |
746 | GeoMagDec = 0; |
747 | } |
747 | } |
748 | else |
748 | else |
749 | { |
749 | { |
750 | FC.FromFC_DisableDeclination = 0; |
750 | FC.FromFC_DisableDeclination = 0; |
751 | FC.FromFC_CompassOffset = 10 * (signed char) FromFlightCtrl.Param.Byte[7]; |
751 | FC.FromFC_CompassOffset = 10 * (signed char) FromFlightCtrl.Param.Byte[7]; |
752 | } |
752 | } |
753 | Parameter.GlobalConfig = FromFlightCtrl.Param.Byte[8]; |
753 | Parameter.GlobalConfig = FromFlightCtrl.Param.Byte[8]; |
754 | Parameter.ExtraConfig = FromFlightCtrl.Param.Byte[9]; |
754 | Parameter.ExtraConfig = FromFlightCtrl.Param.Byte[9]; |
755 | Parameter.OrientationAngle = FromFlightCtrl.Param.Byte[10]; |
755 | Parameter.OrientationAngle = FromFlightCtrl.Param.Byte[10]; |
756 | Parameter.GlobalConfig3 = FromFlightCtrl.Param.Byte[11]; |
756 | Parameter.GlobalConfig3 = FromFlightCtrl.Param.Byte[11]; |
757 | DebugOut.StatusGreen |= AMPEL_FC; // status of FC Present |
757 | DebugOut.StatusGreen |= AMPEL_FC; // status of FC Present |
758 | DebugOut.StatusGreen |= AMPEL_BL; // status of BL Present |
758 | DebugOut.StatusGreen |= AMPEL_BL; // status of BL Present |
759 | if(FC.Error[0] || FC.Error[1] /* || FC.Error[2] || FC.Error[3] || FC.Error[4]*/) DebugOut.StatusRed |= AMPEL_FC; |
759 | if(FC.Error[0] || FC.Error[1] /* || FC.Error[2] || FC.Error[3] || FC.Error[4]*/) DebugOut.StatusRed |= AMPEL_FC; |
760 | else DebugOut.StatusRed &= ~AMPEL_FC; |
760 | else DebugOut.StatusRed &= ~AMPEL_FC; |
761 | break; |
761 | break; |
762 | default: |
762 | default: |
763 | break; |
763 | break; |
764 | } |
764 | } |
765 | DebugOut.Analog[0] = FromFlightCtrl.AngleNick; |
765 | DebugOut.Analog[0] = FromFlightCtrl.AngleNick; |
766 | DebugOut.Analog[1] = FromFlightCtrl.AngleRoll; |
766 | DebugOut.Analog[1] = FromFlightCtrl.AngleRoll; |
767 | DebugOut.Analog[2] = FromFlightCtrl.AccNick; |
767 | DebugOut.Analog[2] = FromFlightCtrl.AccNick; |
768 | DebugOut.Analog[3] = FromFlightCtrl.AccRoll; |
768 | DebugOut.Analog[3] = FromFlightCtrl.AccRoll; |
769 | DebugOut.Analog[11] = FromFlightCtrl.GyroHeading/10;// in deg |
769 | DebugOut.Analog[11] = FromFlightCtrl.GyroHeading/10;// in deg |
770 | Data3D.AngleNick = FromFlightCtrl.AngleNick; // in 0.1 deg |
770 | Data3D.AngleNick = FromFlightCtrl.AngleNick; // in 0.1 deg |
771 | Data3D.AngleRoll = FromFlightCtrl.AngleRoll; // in 0.1 deg |
771 | Data3D.AngleRoll = FromFlightCtrl.AngleRoll; // in 0.1 deg |
772 | Data3D.Heading = FromFlightCtrl.GyroHeading; // in 0.1 deg |
772 | Data3D.Heading = FromFlightCtrl.GyroHeading; // in 0.1 deg |
773 | // every time we got new data from the FC via SPI call the navigation routine |
773 | // every time we got new data from the FC via SPI call the navigation routine |
774 | // and update GPSStick that are returned to FC |
774 | // and update GPSStick that are returned to FC |
775 | SPI_RxBuffer_Request = 0; |
775 | SPI_RxBuffer_Request = 0; |
776 | GPS_Navigation(&GPSData, &(ToFlightCtrl.GPSStick)); |
776 | GPS_Navigation(&GPSData, &(ToFlightCtrl.GPSStick)); |
777 | ClearFCStatusFlags = 1; |
777 | ClearFCStatusFlags = 1; |
778 | if(counter) |
778 | if(counter) |
779 | { |
779 | { |
780 | counter--; // count down to enable servo |
780 | counter--; // count down to enable servo |
781 | if(!counter) TIMER2_Init(); // enable Servo Output |
781 | if(!counter) TIMER2_Init(); // enable Servo Output |
782 | } |
782 | } |
783 | timeout = SetDelay(80); // 80 ms, new data are send every 20 ms |
783 | timeout = SetDelay(80); // 80 ms, new data are send every 20 ms |
784 | 784 | ||
785 | } // EOF if(SPI_RxBuffer_Request) |
785 | } // EOF if(SPI_RxBuffer_Request) |
786 | else // no new SPI data |
786 | else // no new SPI data |
787 | { |
787 | { |
788 | if(CheckDelay(timeout) && (counter == 0)) |
788 | if(CheckDelay(timeout) && (counter == 0)) |
789 | { |
789 | { |
790 | TIMER2_Deinit(); // disable Servo Output |
790 | TIMER2_Deinit(); // disable Servo Output |
791 | counter = 50; // reset counter for enabling Servo Output |
791 | counter = 50; // reset counter for enabling Servo Output |
792 | } |
792 | } |
793 | } |
793 | } |
794 | } |
794 | } |
795 | 795 | ||
796 | //------------------------------------------------------ |
796 | //------------------------------------------------------ |
797 | void SPI0_GetFlightCtrlVersion(void) |
797 | void SPI0_GetFlightCtrlVersion(void) |
798 | { |
798 | { |
799 | u32 timeout; |
799 | u32 timeout; |
800 | u8 repeat; |
800 | u8 repeat; |
801 | u8 msg[64]; |
801 | u8 msg[64]; |
802 | 802 | ||
803 | UART1_PutString("\r\n Looking for FlightControl"); |
803 | UART1_PutString("\r\n Looking for FlightControl"); |
804 | FC_Version.Major = 0xFF; |
804 | FC_Version.Major = 0xFF; |
805 | FC_Version.Minor = 0xFF; |
805 | FC_Version.Minor = 0xFF; |
806 | FC_Version.Patch = 0xFF; |
806 | FC_Version.Patch = 0xFF; |
807 | FC_Version.Compatible = 0xFF; |
807 | FC_Version.Compatible = 0xFF; |
808 | 808 | ||
809 | // polling FC version info |
809 | // polling FC version info |
810 | repeat = 0; |
810 | repeat = 0; |
811 | do |
811 | do |
812 | { |
812 | { |
813 | timeout = SetDelay(250); |
813 | timeout = SetDelay(250); |
814 | do |
814 | do |
815 | { |
815 | { |
816 | SPI0_UpdateBuffer(); |
816 | SPI0_UpdateBuffer(); |
817 | if (FC_Version.Major != 0xFF) break; |
817 | if (FC_Version.Major != 0xFF) break; |
818 | }while (!CheckDelay(timeout)); |
818 | }while (!CheckDelay(timeout)); |
819 | UART1_PutString("."); |
819 | UART1_PutString("."); |
820 | repeat++; |
820 | repeat++; |
821 | // FCCalibActive = 1; |
821 | // FCCalibActive = 1; |
822 | }while((FC_Version.Major == 0xFF) && (repeat < 40)); // 40*250ms = 10s |
822 | }while((FC_Version.Major == 0xFF) && (repeat < 40)); // 40*250ms = 10s |
823 | // if we got it |
823 | // if we got it |
824 | if (FC_Version.Major != 0xFF) |
824 | if (FC_Version.Major != 0xFF) |
825 | { |
825 | { |
826 | sprintf(msg, " FC V%d.%d%c HW:%d.%d", FC_Version.Major, FC_Version.Minor, 'a'+FC_Version.Patch, FC_Version.Hardware/10,FC_Version.Hardware%10); |
826 | sprintf(msg, " FC V%d.%2d%c HW:%d.%d", FC_Version.Major, FC_Version.Minor, 'a'+FC_Version.Patch, FC_Version.Hardware/10,FC_Version.Hardware%10); |
827 | UART1_PutString(msg); |
827 | UART1_PutString(msg); |
828 | } |
828 | } |
829 | else UART1_PutString("\n\r not found!"); |
829 | else UART1_PutString("\n\r not found!"); |
830 | } |
830 | } |
831 | 831 | ||
832 | 832 | ||
833 | 833 |