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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 | 73 | ||
74 | #define SPI_RXSYNCBYTE1 0xAA |
74 | #define SPI_RXSYNCBYTE1 0xAA |
75 | #define SPI_RXSYNCBYTE2 0x83 |
75 | #define SPI_RXSYNCBYTE2 0x83 |
76 | #define SPI_TXSYNCBYTE1 0x81 |
76 | #define SPI_TXSYNCBYTE1 0x81 |
77 | #define SPI_TXSYNCBYTE2 0x55 |
77 | #define SPI_TXSYNCBYTE2 0x55 |
78 | 78 | ||
79 | //communication packets |
79 | //communication packets |
80 | FromFlightCtrl_t FromFlightCtrl; |
80 | FromFlightCtrl_t FromFlightCtrl; |
81 | ToFlightCtrl_t ToFlightCtrl; |
81 | ToFlightCtrl_t ToFlightCtrl; |
82 | #define SPI0_TIMEOUT 2500 //ms |
82 | #define SPI0_TIMEOUT 2500 //ms |
83 | volatile u32 SPI0_Timeout = 0; |
83 | volatile u32 SPI0_Timeout = 0; |
84 | u8 Logging_FCStatusFlags1 = 0,Logging_FCStatusFlags2 = 0; |
84 | u8 Logging_FCStatusFlags1 = 0,Logging_FCStatusFlags2 = 0; |
85 | u8 SpeakHoTT = 0; |
85 | u8 SpeakHoTT = 0; |
86 | 86 | ||
87 | // tx packet buffer |
87 | // tx packet buffer |
88 | #define SPI_TXBUFFER_LEN (2 + sizeof(ToFlightCtrl)) // 2 bytes at start are for synchronization |
88 | #define SPI_TXBUFFER_LEN (2 + sizeof(ToFlightCtrl)) // 2 bytes at start are for synchronization |
89 | volatile u8 SPI_TxBuffer[SPI_TXBUFFER_LEN + 10]; |
89 | volatile u8 SPI_TxBuffer[SPI_TXBUFFER_LEN + 10]; |
90 | volatile u8 SPI_TxBufferIndex = 0; |
90 | volatile u8 SPI_TxBufferIndex = 0; |
91 | u8 *Ptr_TxChksum = NULL ; // pointer to checksum in TxBuffer |
91 | u8 *Ptr_TxChksum = NULL ; // pointer to checksum in TxBuffer |
92 | 92 | ||
93 | // rx packet buffer |
93 | // rx packet buffer |
94 | #define SPI_RXBUFFER_LEN sizeof(FromFlightCtrl) |
94 | #define SPI_RXBUFFER_LEN sizeof(FromFlightCtrl) |
95 | volatile u8 SPI_RxBuffer[SPI_RXBUFFER_LEN+10]; |
95 | volatile u8 SPI_RxBuffer[SPI_RXBUFFER_LEN+10]; |
96 | volatile u8 SPI_RxBufferIndex = 0; |
96 | volatile u8 SPI_RxBufferIndex = 0; |
97 | volatile u8 SPI_RxBuffer_Request = 0; |
97 | volatile u8 SPI_RxBuffer_Request = 0; |
98 | #define SPI_COMMAND_INDEX 0 |
98 | #define SPI_COMMAND_INDEX 0 |
99 | 99 | ||
100 | s32 Kalman_K = 32; |
100 | s32 Kalman_K = 32; |
101 | s32 Kalman_MaxDrift = 5 * 16; |
101 | s32 Kalman_MaxDrift = 5 * 16; |
102 | s32 Kalman_MaxFusion = 64; |
102 | s32 Kalman_MaxFusion = 64; |
103 | s32 Kalman_Kompass = 32; |
103 | s32 Kalman_Kompass = 32; |
104 | s32 ToFcGpsZ = 0; |
104 | s32 ToFcGpsZ = 0; |
105 | u8 CompassCalState = 0; |
105 | u8 CompassCalState = 0; |
106 | 106 | ||
107 | 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 }; |
107 | 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_CommandCounter = 0; |
108 | u8 SPI_CommandCounter = 0; |
109 | s32 ToFC_Rotate_C = 64, ToFC_Rotate_S = 0; |
109 | s32 ToFC_Rotate_C = 64, ToFC_Rotate_S = 0; |
110 | s32 HeadFreeStartAngle = 0; |
110 | s32 HeadFreeStartAngle = 0; |
111 | s16 FC_WP_EventChannel = 0, LogFC_WP_EventChannel = 0; // gibt einen Schaltkanal an die FC weiter, wenn der Wegpunkt erreicht wurde |
111 | s16 FC_WP_EventChannel = 0, LogFC_WP_EventChannel = 0; // gibt einen Schaltkanal an die FC weiter, wenn der Wegpunkt erreicht wurde |
112 | u32 ToFC_AltitudeRate = 0; |
112 | u32 ToFC_AltitudeRate = 0; |
113 | s32 ToFC_AltitudeSetpoint = 0; |
113 | s32 ToFC_AltitudeSetpoint = 0; |
114 | u8 FromFC_VarioCharacter = ' '; |
114 | u8 FromFC_VarioCharacter = ' '; |
115 | u8 GPS_Aid_StickMultiplikator = 0; |
115 | u8 GPS_Aid_StickMultiplikator = 0; |
116 | u8 NC_GPS_ModeCharacter = ' '; |
116 | u8 NC_GPS_ModeCharacter = ' '; |
117 | u8 FCCalibActive = 0; |
117 | u8 FCCalibActive = 0; |
118 | u8 FC_is_Calibrated = 0; |
118 | u8 FC_is_Calibrated = 0; |
119 | Motor_t Motor[12]; |
119 | Motor_t Motor[12]; |
120 | u8 NC_To_FC_Flags = 0; |
120 | u8 NC_To_FC_Flags = 0; |
121 | u8 BL_MinOfMaxPWM; // indication if all BL-controllers run on full power |
121 | u8 BL_MinOfMaxPWM; // indication if all BL-controllers run on full power |
122 | u32 FC_I2C_ErrorConter; |
122 | u32 FC_I2C_ErrorConter; |
123 | SPI_Version_t FC_Version; |
123 | SPI_Version_t FC_Version; |
124 | s16 POI_KameraNick = 0; |
124 | s16 POI_KameraNick = 0; |
125 | 125 | ||
126 | //-------------------------------------------------------------- |
126 | //-------------------------------------------------------------- |
127 | void SSP0_IRQHandler(void) |
127 | void SSP0_IRQHandler(void) |
128 | { |
128 | { |
129 | static u8 rxchksum = 0; |
129 | static u8 rxchksum = 0; |
130 | u8 rxdata; |
130 | u8 rxdata; |
131 | 131 | ||
132 | #define SPI_SYNC1 0 |
132 | #define SPI_SYNC1 0 |
133 | #define SPI_SYNC2 1 |
133 | #define SPI_SYNC2 1 |
134 | #define SPI_DATA 2 |
134 | #define SPI_DATA 2 |
135 | static u8 SPI_State = SPI_SYNC1; |
135 | static u8 SPI_State = SPI_SYNC1; |
136 | //IENABLE; |
136 | //IENABLE; |
137 | 137 | ||
138 | // clear pending bits |
138 | // clear pending bits |
139 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxTimeOut); |
139 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxTimeOut); |
140 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxFifo); |
140 | SSP_ClearITPendingBit(SSP0, SSP_IT_RxFifo); |
141 | 141 | ||
142 | // while RxFIFO not empty |
142 | // while RxFIFO not empty |
143 | while(SSP_GetFlagStatus(SSP0, SSP_FLAG_RxFifoNotEmpty) == SET) |
143 | while(SSP_GetFlagStatus(SSP0, SSP_FLAG_RxFifoNotEmpty) == SET) |
144 | { |
144 | { |
145 | rxdata = SSP0->DR; // catch the received byte |
145 | rxdata = SSP0->DR; // catch the received byte |
146 | // Fill TxFIFO while its not full or end of packet is reached |
146 | // Fill TxFIFO while its not full or end of packet is reached |
147 | while (SSP_GetFlagStatus(SSP0, SSP_FLAG_TxFifoNotFull) == SET) |
147 | while (SSP_GetFlagStatus(SSP0, SSP_FLAG_TxFifoNotFull) == SET) |
148 | { |
148 | { |
149 | if (SPI_TxBufferIndex < SPI_TXBUFFER_LEN) // still data to send ? |
149 | if (SPI_TxBufferIndex < SPI_TXBUFFER_LEN) // still data to send ? |
150 | { |
150 | { |
151 | SSP0->DR = SPI_TxBuffer[SPI_TxBufferIndex]; // send a byte |
151 | SSP0->DR = SPI_TxBuffer[SPI_TxBufferIndex]; // send a byte |
152 | *Ptr_TxChksum += SPI_TxBuffer[SPI_TxBufferIndex]; // update checksum |
152 | *Ptr_TxChksum += SPI_TxBuffer[SPI_TxBufferIndex]; // update checksum |
153 | if(SPIWatchDog == 0) *Ptr_TxChksum += 1; // disturbe this packet to stop the communication! |
153 | if(SPIWatchDog == 0) *Ptr_TxChksum += 1; // disturbe this packet to stop the communication! |
154 | SPI_TxBufferIndex++; // pointer to next byte |
154 | SPI_TxBufferIndex++; // pointer to next byte |
155 | } |
155 | } |
156 | else // end of packet is reached reset and copy data to tx buffer |
156 | else // end of packet is reached reset and copy data to tx buffer |
157 | { |
157 | { |
158 | SPI_TxBufferIndex = 0; // reset buffer index |
158 | SPI_TxBufferIndex = 0; // reset buffer index |
159 | ToFlightCtrl.Chksum = 0; // initialize checksum |
159 | ToFlightCtrl.Chksum = 0; // initialize checksum |
160 | ToFlightCtrl.BeepTime = BeepTime; // set beeptime |
160 | ToFlightCtrl.BeepTime = BeepTime; // set beeptime |
161 | BeepTime = 0; // reset local beeptime |
161 | BeepTime = 0; // reset local beeptime |
162 | // copy contents of ToFlightCtrl->SPI_TxBuffer |
162 | // copy contents of ToFlightCtrl->SPI_TxBuffer |
163 | memcpy((u8 *) &(SPI_TxBuffer[2]), (u8 *) &ToFlightCtrl, sizeof(ToFlightCtrl)); |
163 | memcpy((u8 *) &(SPI_TxBuffer[2]), (u8 *) &ToFlightCtrl, sizeof(ToFlightCtrl)); |
164 | } |
164 | } |
165 | } |
165 | } |
166 | switch (SPI_State) |
166 | switch (SPI_State) |
167 | { |
167 | { |
168 | case SPI_SYNC1: |
168 | case SPI_SYNC1: |
169 | SPI_RxBufferIndex = 0; // reset buffer index |
169 | SPI_RxBufferIndex = 0; // reset buffer index |
170 | rxchksum = rxdata; // init checksum |
170 | rxchksum = rxdata; // init checksum |
171 | if (rxdata == SPI_RXSYNCBYTE1) |
171 | if (rxdata == SPI_RXSYNCBYTE1) |
172 | { // 1st syncbyte ok |
172 | { // 1st syncbyte ok |
173 | SPI_State = SPI_SYNC2; // step to sync2 |
173 | SPI_State = SPI_SYNC2; // step to sync2 |
174 | } |
174 | } |
175 | break; |
175 | break; |
176 | case SPI_SYNC2: |
176 | case SPI_SYNC2: |
177 | if (rxdata == SPI_RXSYNCBYTE2) |
177 | if (rxdata == SPI_RXSYNCBYTE2) |
178 | { // 2nd Syncbyte ok |
178 | { // 2nd Syncbyte ok |
179 | rxchksum += rxdata; |
179 | rxchksum += rxdata; |
180 | SPI_State = SPI_DATA; |
180 | SPI_State = SPI_DATA; |
181 | } // 2nd Syncbyte does not match |
181 | } // 2nd Syncbyte does not match |
182 | else |
182 | else |
183 | { |
183 | { |
184 | SPI_State = SPI_SYNC1; //jump back to sync1 |
184 | SPI_State = SPI_SYNC1; //jump back to sync1 |
185 | } |
185 | } |
186 | break; |
186 | break; |
187 | case SPI_DATA: |
187 | case SPI_DATA: |
188 | SPI_RxBuffer[SPI_RxBufferIndex++]= rxdata; // copy databyte to rx buffer |
188 | SPI_RxBuffer[SPI_RxBufferIndex++]= rxdata; // copy databyte to rx buffer |
189 | if(SPI_RxBufferIndex >= SPI_RXBUFFER_LEN) // end of packet is reached |
189 | if(SPI_RxBufferIndex >= SPI_RXBUFFER_LEN) // end of packet is reached |
190 | { |
190 | { |
191 | if (rxdata == rxchksum) // verify checksum byte |
191 | if (rxdata == rxchksum) // verify checksum byte |
192 | { |
192 | { |
193 | // copy SPI_RxBuffer -> FromFlightCtrl |
193 | // copy SPI_RxBuffer -> FromFlightCtrl |
194 | if(!SPI_RxBuffer_Request) // block writing to FromFlightCtrl on reading access |
194 | if(!SPI_RxBuffer_Request) // block writing to FromFlightCtrl on reading access |
195 | { |
195 | { |
196 | memcpy((u8 *) &FromFlightCtrl, (u8 *) SPI_RxBuffer, sizeof(FromFlightCtrl)); |
196 | memcpy((u8 *) &FromFlightCtrl, (u8 *) SPI_RxBuffer, sizeof(FromFlightCtrl)); |
197 | SPI_RxBuffer_Request = 1; |
197 | SPI_RxBuffer_Request = 1; |
198 | } |
198 | } |
199 | // reset timeout counter on good packet |
199 | // reset timeout counter on good packet |
200 | SPI0_Timeout = SetDelay(SPI0_TIMEOUT); |
200 | SPI0_Timeout = SetDelay(SPI0_TIMEOUT); |
201 | DebugOut.Analog[13]++; |
201 | DebugOut.Analog[13]++; |
202 | } |
202 | } |
203 | else // bad checksum byte |
203 | else // bad checksum byte |
204 | { |
204 | { |
205 | DebugOut.Analog[12]++; // increase SPI chksum error counter |
205 | DebugOut.Analog[12]++; // increase SPI chksum error counter |
206 | } |
206 | } |
207 | SPI_State = SPI_SYNC1; // reset state |
207 | SPI_State = SPI_SYNC1; // reset state |
208 | } |
208 | } |
209 | else // end of packet not reached |
209 | else // end of packet not reached |
210 | { |
210 | { |
211 | rxchksum += rxdata; // update checksum |
211 | rxchksum += rxdata; // update checksum |
212 | } |
212 | } |
213 | break; |
213 | break; |
214 | default: |
214 | default: |
215 | SPI_State = SPI_SYNC1; |
215 | SPI_State = SPI_SYNC1; |
216 | break; |
216 | break; |
217 | } |
217 | } |
218 | } |
218 | } |
219 | 219 | ||
220 | // IDISABLE; |
220 | // IDISABLE; |
221 | VIC1->VAR = 0xFF; // write any value to VIC0 Vector address register |
221 | VIC1->VAR = 0xFF; // write any value to VIC0 Vector address register |
222 | } |
222 | } |
223 | 223 | ||
224 | //-------------------------------------------------------------- |
224 | //-------------------------------------------------------------- |
225 | void SPI0_Init(void) |
225 | void SPI0_Init(void) |
226 | { |
226 | { |
227 | GPIO_InitTypeDef GPIO_InitStructure; |
227 | GPIO_InitTypeDef GPIO_InitStructure; |
228 | SSP_InitTypeDef SSP_InitStructure; |
228 | SSP_InitTypeDef SSP_InitStructure; |
229 | 229 | ||
230 | UART1_PutString("\r\n SPI init..."); |
230 | UART1_PutString("\r\n SPI init..."); |
231 | 231 | ||
232 | SCU_APBPeriphClockConfig(__GPIO2 ,ENABLE); |
232 | SCU_APBPeriphClockConfig(__GPIO2 ,ENABLE); |
233 | SCU_APBPeriphClockConfig(__SSP0 ,ENABLE); |
233 | SCU_APBPeriphClockConfig(__SSP0 ,ENABLE); |
234 | 234 | ||
235 | GPIO_DeInit(GPIO2); |
235 | GPIO_DeInit(GPIO2); |
236 | //SSP0_CLK, SSP0_MOSI, SSP0_NSS pins |
236 | //SSP0_CLK, SSP0_MOSI, SSP0_NSS pins |
237 | GPIO_StructInit(&GPIO_InitStructure); |
237 | GPIO_StructInit(&GPIO_InitStructure); |
238 | GPIO_InitStructure.GPIO_Direction = GPIO_PinInput; |
238 | GPIO_InitStructure.GPIO_Direction = GPIO_PinInput; |
239 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_4 | GPIO_Pin_5 | GPIO_Pin_7; |
239 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_4 | GPIO_Pin_5 | GPIO_Pin_7; |
240 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
240 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
241 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
241 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
242 | GPIO_InitStructure.GPIO_Alternate = GPIO_InputAlt1; //SSP0_SCLK, SSP0_MOSI, SSP0_NSS |
242 | GPIO_InitStructure.GPIO_Alternate = GPIO_InputAlt1; //SSP0_SCLK, SSP0_MOSI, SSP0_NSS |
243 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
243 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
244 | 244 | ||
245 | // SSP0_MISO pin GPIO2.6 |
245 | // SSP0_MISO pin GPIO2.6 |
246 | GPIO_StructInit(&GPIO_InitStructure); |
246 | GPIO_StructInit(&GPIO_InitStructure); |
247 | GPIO_InitStructure.GPIO_Direction = GPIO_PinOutput; |
247 | GPIO_InitStructure.GPIO_Direction = GPIO_PinOutput; |
248 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_6; |
248 | GPIO_InitStructure.GPIO_Pin = GPIO_Pin_6; |
249 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
249 | GPIO_InitStructure.GPIO_Type = GPIO_Type_PushPull ; |
250 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
250 | GPIO_InitStructure.GPIO_IPInputConnected = GPIO_IPInputConnected_Enable; |
251 | GPIO_InitStructure.GPIO_Alternate = GPIO_OutputAlt2; //SSP0_MISO |
251 | GPIO_InitStructure.GPIO_Alternate = GPIO_OutputAlt2; //SSP0_MISO |
252 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
252 | GPIO_Init (GPIO2, &GPIO_InitStructure); |
253 | 253 | ||
254 | SSP_DeInit(SSP0); |
254 | SSP_DeInit(SSP0); |
255 | SSP_StructInit(&SSP_InitStructure); |
255 | SSP_StructInit(&SSP_InitStructure); |
256 | SSP_InitStructure.SSP_FrameFormat = SSP_FrameFormat_Motorola; |
256 | SSP_InitStructure.SSP_FrameFormat = SSP_FrameFormat_Motorola; |
257 | SSP_InitStructure.SSP_Mode = SSP_Mode_Slave; |
257 | SSP_InitStructure.SSP_Mode = SSP_Mode_Slave; |
258 | SSP_InitStructure.SSP_SlaveOutput = SSP_SlaveOutput_Enable; |
258 | SSP_InitStructure.SSP_SlaveOutput = SSP_SlaveOutput_Enable; |
259 | SSP_InitStructure.SSP_CPHA = SSP_CPHA_1Edge; |
259 | SSP_InitStructure.SSP_CPHA = SSP_CPHA_1Edge; |
260 | SSP_InitStructure.SSP_CPOL = SSP_CPOL_Low; |
260 | SSP_InitStructure.SSP_CPOL = SSP_CPOL_Low; |
261 | SSP_InitStructure.SSP_ClockRate = 0; |
261 | SSP_InitStructure.SSP_ClockRate = 0; |
262 | 262 | ||
263 | SSP_Init(SSP0, &SSP_InitStructure); |
263 | SSP_Init(SSP0, &SSP_InitStructure); |
264 | SSP_ITConfig(SSP0, SSP_IT_RxFifo | SSP_IT_RxTimeOut, ENABLE); |
264 | SSP_ITConfig(SSP0, SSP_IT_RxFifo | SSP_IT_RxTimeOut, ENABLE); |
265 | SSP_Cmd(SSP0, ENABLE); |
265 | SSP_Cmd(SSP0, ENABLE); |
266 | // initialize the syncbytes in the tx buffer |
266 | // initialize the syncbytes in the tx buffer |
267 | SPI_TxBuffer[0] = SPI_TXSYNCBYTE1; |
267 | SPI_TxBuffer[0] = SPI_TXSYNCBYTE1; |
268 | SPI_TxBuffer[1] = SPI_TXSYNCBYTE2; |
268 | SPI_TxBuffer[1] = SPI_TXSYNCBYTE2; |
269 | // set the pointer to the checksum byte in the tx buffer |
269 | // set the pointer to the checksum byte in the tx buffer |
270 | Ptr_TxChksum = (u8 *) &(((ToFlightCtrl_t *) &(SPI_TxBuffer[2]))->Chksum); |
270 | Ptr_TxChksum = (u8 *) &(((ToFlightCtrl_t *) &(SPI_TxBuffer[2]))->Chksum); |
271 | 271 | ||
272 | ToFlightCtrl.GPSStick.Nick = 0; |
272 | ToFlightCtrl.GPSStick.Nick = 0; |
273 | ToFlightCtrl.GPSStick.Roll = 0; |
273 | ToFlightCtrl.GPSStick.Roll = 0; |
274 | // ToFlightCtrl.GPSStick.Yaw = 0; |
274 | // ToFlightCtrl.GPSStick.Yaw = 0; |
275 | 275 | ||
276 | VIC_Config(SSP0_ITLine, VIC_IRQ, PRIORITY_SPI0); |
276 | VIC_Config(SSP0_ITLine, VIC_IRQ, PRIORITY_SPI0); |
277 | VIC_ITCmd(SSP0_ITLine, ENABLE); |
277 | VIC_ITCmd(SSP0_ITLine, ENABLE); |
278 | 278 | ||
279 | SPI0_Timeout = SetDelay(4*SPI0_TIMEOUT); |
279 | SPI0_Timeout = SetDelay(4*SPI0_TIMEOUT); |
280 | 280 | ||
281 | UART1_PutString("ok"); |
281 | UART1_PutString("ok"); |
282 | } |
282 | } |
283 | 283 | ||
284 | 284 | ||
285 | //------------------------------------------------------ |
285 | //------------------------------------------------------ |
286 | void SPI0_UpdateBuffer(void) |
286 | void SPI0_UpdateBuffer(void) |
287 | { |
287 | { |
288 | static u32 timeout = 0; |
288 | static u32 timeout = 0; |
289 | static u8 counter = 50,hott_index = 0, last_error_code = 0, enable_injecting = 0; |
289 | static u8 counter = 50,hott_index = 0, last_error_code = 0, enable_injecting = 0; |
290 | static s16 last_wp_event = 0; |
290 | static s16 last_wp_event = 0; |
291 | s16 tmp; |
291 | s16 tmp; |
292 | s32 i1,i2; |
292 | s32 i1,i2; |
293 | 293 | ||
294 | SPIWatchDog = 3500; // stop communication to FC after this timeout |
294 | SPIWatchDog = 3500; // stop communication to FC after this timeout |
295 | if(SPI_RxBuffer_Request) |
295 | if(SPI_RxBuffer_Request) |
296 | { |
296 | { |
297 | // avoid sending data via SPI during the update of the ToFlightCtrl structure |
297 | // avoid sending data via SPI during the update of the ToFlightCtrl structure |
298 | VIC_ITCmd(SSP0_ITLine, DISABLE); // disable SPI interrupt |
298 | VIC_ITCmd(SSP0_ITLine, DISABLE); // disable SPI interrupt |
299 | ToFlightCtrl.CompassHeading = Compass_Heading; |
299 | ToFlightCtrl.CompassHeading = Compass_Heading; |
300 | DebugOut.Analog[10] = ToFlightCtrl.CompassHeading; |
300 | DebugOut.Analog[10] = ToFlightCtrl.CompassHeading; |
301 | if(ToFlightCtrl.CompassHeading >= 0) ToFlightCtrl.CompassHeading = (360 + ToFlightCtrl.CompassHeading + FromFlightCtrl.GyroYaw / 12) % 360; |
301 | if(ToFlightCtrl.CompassHeading >= 0) ToFlightCtrl.CompassHeading = (360 + ToFlightCtrl.CompassHeading + FromFlightCtrl.GyroYaw / 12) % 360; |
302 | ToFlightCtrl.MagVecX = MagVector.X; |
302 | ToFlightCtrl.MagVecX = MagVector.X; |
303 | ToFlightCtrl.MagVecY = MagVector.Y; |
303 | ToFlightCtrl.MagVecY = MagVector.Y; |
304 | ToFlightCtrl.MagVecZ = MagVector.Z; |
304 | ToFlightCtrl.MagVecZ = MagVector.Z; |
305 | // ToFlightCtrl.NCStatus = 0; |
305 | // ToFlightCtrl.NCStatus = 0; |
306 | // cycle spi commands |
306 | // cycle spi commands |
307 | if(ErrorCode != last_error_code && enable_injecting) |
307 | if(ErrorCode != last_error_code && enable_injecting) |
308 | { |
308 | { |
309 | ToFlightCtrl.Command = SPI_NCCMD_VERSION; |
309 | ToFlightCtrl.Command = SPI_NCCMD_VERSION; |
310 | last_error_code = ErrorCode; |
310 | last_error_code = ErrorCode; |
311 | enable_injecting = 0; |
311 | enable_injecting = 0; |
312 | } |
312 | } |
313 | else |
313 | else |
314 | if(FC_WP_EventChannel != last_wp_event && enable_injecting) |
314 | if(FC_WP_EventChannel != last_wp_event && enable_injecting) |
315 | { |
315 | { |
316 | ToFlightCtrl.Command = SPI_NCCMD_GPSINFO; |
316 | ToFlightCtrl.Command = SPI_NCCMD_GPSINFO; |
317 | last_wp_event = FC_WP_EventChannel; |
317 | last_wp_event = FC_WP_EventChannel; |
318 | enable_injecting = 0; |
318 | enable_injecting = 0; |
319 | } |
319 | } |
320 | else |
320 | else |
321 | { |
321 | { |
322 | ToFlightCtrl.Command = SPI_CommandSequence[SPI_CommandCounter++]; |
322 | ToFlightCtrl.Command = SPI_CommandSequence[SPI_CommandCounter++]; |
323 | // restart command cycle at the end |
323 | // restart command cycle at the end |
324 | if(SPI_CommandCounter >= sizeof(SPI_CommandSequence)) SPI_CommandCounter = 0; |
324 | if(SPI_CommandCounter >= sizeof(SPI_CommandSequence)) SPI_CommandCounter = 0; |
325 | if(ToFlightCtrl.Command == SPI_NCCMD_KALMAN) enable_injecting = 1; |
325 | if(ToFlightCtrl.Command == SPI_NCCMD_KALMAN) enable_injecting = 1; |
326 | } |
326 | } |
327 | 327 | ||
328 | #define FLAG_GPS_AID 0x01 |
328 | #define FLAG_GPS_AID 0x01 |
329 | switch (ToFlightCtrl.Command) |
329 | switch (ToFlightCtrl.Command) |
330 | { |
330 | { |
331 | case SPI_NCCMD_KALMAN: // wird am häufigsten betätigt |
331 | case SPI_NCCMD_KALMAN: // wird am häufigsten betätigt |
332 | ToFlightCtrl.Param.sByte[0] = (s8) Kalman_K; |
332 | ToFlightCtrl.Param.sByte[0] = (s8) Kalman_K; |
333 | ToFlightCtrl.Param.sByte[1] = (s8) Kalman_MaxFusion; |
333 | ToFlightCtrl.Param.sByte[1] = (s8) Kalman_MaxFusion; |
334 | ToFlightCtrl.Param.sByte[2] = (s8) Kalman_MaxDrift; |
334 | ToFlightCtrl.Param.sByte[2] = (s8) Kalman_MaxDrift; |
335 | ToFlightCtrl.Param.Byte[3] = (u8) Kalman_Kompass; |
335 | ToFlightCtrl.Param.Byte[3] = (u8) Kalman_Kompass; |
336 | ToFlightCtrl.Param.sByte[4] = (s8) ToFcGpsZ; |
336 | ToFlightCtrl.Param.sByte[4] = (s8) ToFcGpsZ; |
337 | ToFlightCtrl.Param.Byte[5] = (s8) ToFC_Rotate_C; |
337 | ToFlightCtrl.Param.Byte[5] = (s8) ToFC_Rotate_C; |
338 | ToFlightCtrl.Param.Byte[6] = (s8) ToFC_Rotate_S; |
338 | ToFlightCtrl.Param.Byte[6] = (s8) ToFC_Rotate_S; |
339 | ToFlightCtrl.Param.Byte[7] = GPS_Aid_StickMultiplikator; |
339 | ToFlightCtrl.Param.Byte[7] = GPS_Aid_StickMultiplikator; |
340 | if(CAM_Orientation.UpdateMask & CAM_UPDATE_AZIMUTH) |
340 | if(CAM_Orientation.UpdateMask & CAM_UPDATE_AZIMUTH) |
341 | { |
341 | { |
342 | ToFlightCtrl.Param.sInt[4] = CAM_Orientation.Azimuth; |
342 | ToFlightCtrl.Param.sInt[4] = CAM_Orientation.Azimuth; |
343 | CAM_Orientation.UpdateMask &= ~CAM_UPDATE_AZIMUTH; |
343 | CAM_Orientation.UpdateMask &= ~CAM_UPDATE_AZIMUTH; |
344 | } |
344 | } |
345 | else |
345 | else |
346 | { |
346 | { |
347 | ToFlightCtrl.Param.sInt[4] = -1; |
347 | ToFlightCtrl.Param.sInt[4] = -1; |
348 | } |
348 | } |
349 | 349 | ||
350 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_NEW_CAMERA_ELEVATION, &tmp)) // Elevation set via 'j' command |
350 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_NEW_CAMERA_ELEVATION, &tmp)) // Elevation set via 'j' command |
351 | { |
351 | { |
352 | POI_KameraNick = tmp; |
352 | POI_KameraNick = tmp; |
353 | } |
353 | } |
354 | else |
354 | else |
355 | { |
355 | { |
356 | //if(FC.StatusFlags2 & FC_STATUS2_CAREFREE) // only, if carefree is active |
356 | //if(FC.StatusFlags2 & FC_STATUS2_CAREFREE) // only, if carefree is active |
357 | POI_KameraNick = CAM_Orientation.Elevation; |
357 | POI_KameraNick = CAM_Orientation.Elevation; |
358 | //else ToFlightCtrl.Param.sInt[5] = 0; |
358 | //else ToFlightCtrl.Param.sInt[5] = 0; |
359 | } |
359 | } |
360 | ToFlightCtrl.Param.sInt[5] = POI_KameraNick; |
360 | ToFlightCtrl.Param.sInt[5] = POI_KameraNick; |
361 | break; |
361 | break; |
362 | 362 | ||
363 | case SPI_NCCMD_VERSION: |
363 | case SPI_NCCMD_VERSION: |
364 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
364 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
365 | //+ higher than the maximum allowed altitude |
365 | //+ higher than the maximum allowed altitude |
366 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
366 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
367 | ToFlightCtrl.Param.Byte[0] = VERSION_MAJOR; |
367 | ToFlightCtrl.Param.Byte[0] = VERSION_MAJOR; |
368 | ToFlightCtrl.Param.Byte[1] = VERSION_MINOR; |
368 | ToFlightCtrl.Param.Byte[1] = VERSION_MINOR; |
369 | ToFlightCtrl.Param.Byte[2] = VERSION_PATCH; |
369 | ToFlightCtrl.Param.Byte[2] = VERSION_PATCH; |
370 | ToFlightCtrl.Param.Byte[3] = FC_SPI_COMPATIBLE; |
370 | ToFlightCtrl.Param.Byte[3] = FC_SPI_COMPATIBLE; |
371 | ToFlightCtrl.Param.Byte[4] = Version_HW; |
371 | ToFlightCtrl.Param.Byte[4] = Version_HW; |
372 | ToFlightCtrl.Param.Byte[5] = DebugOut.StatusGreen; |
372 | ToFlightCtrl.Param.Byte[5] = DebugOut.StatusGreen; |
373 | ToFlightCtrl.Param.Byte[6] = DebugOut.StatusRed; |
373 | ToFlightCtrl.Param.Byte[6] = DebugOut.StatusRed; |
374 | ToFlightCtrl.Param.Byte[7] = ErrorCode; // muss in SPI_NCCMD_VERSION bleiben! (siehe oben) |
374 | ToFlightCtrl.Param.Byte[7] = ErrorCode; // muss in SPI_NCCMD_VERSION bleiben! (siehe oben) |
375 | ToFlightCtrl.Param.Byte[8] = NC_GPS_ModeCharacter; |
375 | ToFlightCtrl.Param.Byte[8] = NC_GPS_ModeCharacter; |
376 | ToFlightCtrl.Param.Byte[9] = SerialLinkOkay; |
376 | ToFlightCtrl.Param.Byte[9] = SerialLinkOkay; |
377 | ToFlightCtrl.Param.Byte[10] = NC_To_FC_Flags; |
377 | ToFlightCtrl.Param.Byte[10] = NC_To_FC_Flags; |
378 | if(AbsoluteFlyingAltitude > 255) ToFlightCtrl.Param.Byte[11] = 0; // then the limitation of the FC doesn't work |
378 | if(AbsoluteFlyingAltitude > 255) ToFlightCtrl.Param.Byte[11] = 0; // then the limitation of the FC doesn't work |
379 | else ToFlightCtrl.Param.Byte[11] = AbsoluteFlyingAltitude; |
379 | else ToFlightCtrl.Param.Byte[11] = AbsoluteFlyingAltitude; |
380 | break; |
380 | break; |
381 | case SPI_MISC: |
381 | case SPI_MISC: |
382 | ToFlightCtrl.Param.Byte[0] = EarthMagneticFieldFiltered/5; |
382 | ToFlightCtrl.Param.Byte[0] = EarthMagneticFieldFiltered/5; |
383 | ToFlightCtrl.Param.Byte[1] = EarthMagneticInclination; |
383 | ToFlightCtrl.Param.Byte[1] = EarthMagneticInclination; |
384 | ToFlightCtrl.Param.Byte[2] = EarthMagneticInclinationTheoretic; |
384 | ToFlightCtrl.Param.Byte[2] = EarthMagneticInclinationTheoretic; |
385 | ToFlightCtrl.Param.Byte[3] = SpeakHoTT; |
385 | ToFlightCtrl.Param.Byte[3] = SpeakHoTT; |
386 | ToFlightCtrl.Param.Byte[4] = NaviData.WaypointIndex; // index of current waypoints running from 0 to WaypointNumber-1 |
386 | ToFlightCtrl.Param.Byte[4] = NaviData.WaypointIndex; // index of current waypoints running from 0 to WaypointNumber-1 |
387 | ToFlightCtrl.Param.Byte[5] = NaviData.WaypointNumber; // number of stored waypoints |
387 | ToFlightCtrl.Param.Byte[5] = NaviData.WaypointNumber; // number of stored waypoints |
388 | ToFlightCtrl.Param.Int[3] = NaviData.TargetPositionDeviation.Distance / 10; |
388 | ToFlightCtrl.Param.Int[3] = NaviData.TargetPositionDeviation.Distance / 10; |
389 | ToFlightCtrl.Param.Byte[8] = NaviData.TargetHoldTime; // time in s to stay at the given target, counts down to 0 if target has been reached |
389 | ToFlightCtrl.Param.Byte[8] = NaviData.TargetHoldTime; // time in s to stay at the given target, counts down to 0 if target has been reached |
390 | ToFlightCtrl.Param.Byte[9] = 0; |
390 | ToFlightCtrl.Param.Byte[9] = 0; |
391 | ToFlightCtrl.Param.Byte[10] = 0; |
391 | ToFlightCtrl.Param.Byte[10] = 0; |
392 | ToFlightCtrl.Param.Byte[11] = 0; |
392 | ToFlightCtrl.Param.Byte[11] = 0; |
393 | SpeakHoTT = 0; |
393 | SpeakHoTT = 0; |
394 | break; |
394 | break; |
395 | 395 | ||
396 | case SPI_NCCMD_GPSINFO: |
396 | case SPI_NCCMD_GPSINFO: |
397 | ToFlightCtrl.Param.Byte[0] = GPSData.Flags; |
397 | ToFlightCtrl.Param.Byte[0] = GPSData.Flags; |
398 | ToFlightCtrl.Param.Byte[1] = GPSData.NumOfSats; |
398 | ToFlightCtrl.Param.Byte[1] = GPSData.NumOfSats; |
399 | ToFlightCtrl.Param.Byte[2] = GPSData.SatFix; |
399 | ToFlightCtrl.Param.Byte[2] = GPSData.SatFix; |
400 | ToFlightCtrl.Param.Byte[3] = GPSData.Speed_Ground / 100; // m/s |
400 | ToFlightCtrl.Param.Byte[3] = GPSData.Speed_Ground / 100; // m/s |
401 | ToFlightCtrl.Param.Int[2] = NaviData.HomePositionDeviation.Distance; // dm //4&5 |
401 | ToFlightCtrl.Param.Int[2] = NaviData.HomePositionDeviation.Distance; // dm //4&5 |
402 | ToFlightCtrl.Param.sInt[3] = NaviData.HomePositionDeviation.Bearing; // deg //6&7 |
402 | ToFlightCtrl.Param.sInt[3] = NaviData.HomePositionDeviation.Bearing; // deg //6&7 |
403 | if(FC_WP_EventChannel > 254) FC_WP_EventChannel = 254; // Muss in SPI_NCCMD_GPSINFO bleiben! (siehe oben) |
403 | if(FC_WP_EventChannel > 254) FC_WP_EventChannel = 254; // Muss in SPI_NCCMD_GPSINFO bleiben! (siehe oben) |
404 | if(FC_WP_EventChannel) LogFC_WP_EventChannel = FC_WP_EventChannel; // to make sure that it will be logged |
404 | if(FC_WP_EventChannel) LogFC_WP_EventChannel = FC_WP_EventChannel; // to make sure that it will be logged |
405 | ToFlightCtrl.Param.Byte[8] = (s8)(FC_WP_EventChannel - 127); |
405 | ToFlightCtrl.Param.Byte[8] = (s8)(FC_WP_EventChannel - 127); |
406 | FC_WP_EventChannel = 0; // the GPS-Routine will set it again |
406 | FC_WP_EventChannel = 0; // the GPS-Routine will set it again |
407 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_RATE, &tmp)) |
407 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_RATE, &tmp)) |
408 | { |
408 | { |
409 | ToFlightCtrl.Param.Byte[9] = (u8)tmp; |
409 | ToFlightCtrl.Param.Byte[9] = (u8)tmp; |
410 | } |
410 | } |
411 | else |
411 | else |
412 | { |
412 | { |
413 | ToFlightCtrl.Param.Byte[9] = (u8)ToFC_AltitudeRate; |
413 | ToFlightCtrl.Param.Byte[9] = (u8)ToFC_AltitudeRate; |
414 | } |
414 | } |
415 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_SETPOINT, &tmp)) |
415 | if(NCRARAM_STATE_VALID == NCParams_GetValue(NCPARAMS_ALTITUDE_SETPOINT, &tmp)) |
416 | { |
416 | { |
417 | ToFlightCtrl.Param.sInt[5] = tmp; |
417 | ToFlightCtrl.Param.sInt[5] = tmp; |
418 | } |
418 | } |
419 | else |
419 | else |
420 | { |
420 | { |
421 | ToFlightCtrl.Param.sInt[5] = (s16)ToFC_AltitudeSetpoint; |
421 | ToFlightCtrl.Param.sInt[5] = (s16)ToFC_AltitudeSetpoint; |
422 | } |
422 | } |
423 | break; |
423 | break; |
424 | case SPI_NCCMD_HOTT_INFO: |
424 | case SPI_NCCMD_HOTT_INFO: |
425 | switch(hott_index++) |
425 | switch(hott_index++) |
426 | { |
426 | { |
427 | case 0: |
427 | case 0: |
428 | //Dezimalgrad --> Grad mit Dezimalminuten --> Grad, Minuten, Sekunden |
428 | //Dezimalgrad --> Grad mit Dezimalminuten --> Grad, Minuten, Sekunden |
429 | //53.285788 7.4847269 --> N53° 17.14728 E7° 29.08362 --> N53° 17' 8.837" E7° 29' 5.017" |
429 | //53.285788 7.4847269 --> N53° 17.14728 E7° 29.08362 --> N53° 17' 8.837" E7° 29' 5.017" |
430 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
430 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
431 | ToFlightCtrl.Param.Byte[0] = 3+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
431 | ToFlightCtrl.Param.Byte[0] = 3+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
432 | ToFlightCtrl.Param.Byte[1] = 9-1; // how many |
432 | ToFlightCtrl.Param.Byte[1] = 9-1; // how many |
433 | //----------------------------- |
433 | //----------------------------- |
434 | ToFlightCtrl.Param.Byte[2] = FromFlightCtrl.GyroHeading / 20;//NaviData.HomePositionDeviation.Bearing / 2; |
434 | ToFlightCtrl.Param.Byte[2] = FromFlightCtrl.GyroHeading / 20;//NaviData.HomePositionDeviation.Bearing / 2; |
435 | i1 = GPSData.Speed_Ground; // in cm/sec |
435 | i1 = GPSData.Speed_Ground; // in cm/sec |
436 | i1 *= 36; |
436 | i1 *= 36; |
437 | i1 /= 1000; |
437 | i1 /= 1000; |
438 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
438 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
439 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
439 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
440 | //----------------------------- |
440 | //----------------------------- |
441 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 1; // 1 = S |
441 | if(GPSData.Position.Latitude < 0) ToFlightCtrl.Param.Byte[5] = 1; // 1 = S |
442 | else ToFlightCtrl.Param.Byte[5] = 0; // 1 = S |
442 | else ToFlightCtrl.Param.Byte[5] = 0; // 1 = S |
443 | i1 = abs(GPSData.Position.Latitude)/10000000L; |
443 | i1 = abs(GPSData.Position.Latitude)/10000000L; |
444 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
444 | i2 = abs(GPSData.Position.Latitude)%10000000L; |
445 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
445 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
446 | i1 *= 100; |
446 | i1 *= 100; |
447 | i1 += i2 / 100000; |
447 | i1 += i2 / 100000; |
448 | i2 = i2 % 100000; |
448 | i2 = i2 % 100000; |
449 | i2 /= 10; |
449 | i2 /= 10; |
450 | ToFlightCtrl.Param.Byte[6] = i1 % 256; |
450 | ToFlightCtrl.Param.Byte[6] = i1 % 256; |
451 | ToFlightCtrl.Param.Byte[7] = i1 / 256; |
451 | ToFlightCtrl.Param.Byte[7] = i1 / 256; |
452 | ToFlightCtrl.Param.Byte[8] = i2 % 256; |
452 | ToFlightCtrl.Param.Byte[8] = i2 % 256; |
453 | ToFlightCtrl.Param.Byte[9] = i2 / 256; |
453 | ToFlightCtrl.Param.Byte[9] = i2 / 256; |
454 | break; |
454 | break; |
455 | case 1: |
455 | case 1: |
456 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
456 | ToFlightCtrl.Param.Byte[11] = HOTT_GPS_PACKET_ID; |
457 | ToFlightCtrl.Param.Byte[0] = 11+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
457 | ToFlightCtrl.Param.Byte[0] = 11+3; // index +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
458 | ToFlightCtrl.Param.Byte[1] = 8-1; // how many |
458 | ToFlightCtrl.Param.Byte[1] = 8-1; // how many |
459 | //----------------------------- |
459 | //----------------------------- |
460 | if(GPSData.Position.Longitude < 0) ToFlightCtrl.Param.Byte[2] = 1; // 1 = E |
460 | if(GPSData.Position.Longitude < 0) ToFlightCtrl.Param.Byte[2] = 1; // 1 = E |
461 | else ToFlightCtrl.Param.Byte[2] = 0; // 1 = S |
461 | else ToFlightCtrl.Param.Byte[2] = 0; // 1 = S |
462 | i1 = abs(GPSData.Position.Longitude)/10000000L; |
462 | i1 = abs(GPSData.Position.Longitude)/10000000L; |
463 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
463 | i2 = abs(GPSData.Position.Longitude)%10000000L; |
464 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
464 | if(!(NCFlags & NC_FLAG_GPS_OK)) {i1 = 0; i2 = 0;} |
465 | i1 *= 100; |
465 | i1 *= 100; |
466 | i1 += i2 / 100000; |
466 | i1 += i2 / 100000; |
467 | i2 = i2 % 100000; |
467 | i2 = i2 % 100000; |
468 | i2 /= 10; |
468 | i2 /= 10; |
469 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
469 | ToFlightCtrl.Param.Byte[3] = i1 % 256; |
470 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
470 | ToFlightCtrl.Param.Byte[4] = i1 / 256; |
471 | ToFlightCtrl.Param.Byte[5] = i2 % 256; |
471 | ToFlightCtrl.Param.Byte[5] = i2 % 256; |
472 | ToFlightCtrl.Param.Byte[6] = i2 / 256; |
472 | ToFlightCtrl.Param.Byte[6] = i2 / 256; |
473 | //----------------------------- |
473 | //----------------------------- |
474 | i1 = NaviData.HomePositionDeviation.Distance / 10; // dann in m |
474 | i1 = NaviData.HomePositionDeviation.Distance / 10; // dann in m |
475 | ToFlightCtrl.Param.Byte[7] = i1 % 256; |
475 | ToFlightCtrl.Param.Byte[7] = i1 % 256; |
476 | ToFlightCtrl.Param.Byte[8] = i1 / 256; |
476 | ToFlightCtrl.Param.Byte[8] = i1 / 256; |
477 | break; |
477 | break; |
478 | case 2: |
478 | case 2: |
479 | ToFlightCtrl.Param.Byte[11] = HOTT_GENERAL_PACKET_ID; |
479 | ToFlightCtrl.Param.Byte[11] = HOTT_GENERAL_PACKET_ID; |
480 | ToFlightCtrl.Param.Byte[0] = 5+3; // index // +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
480 | ToFlightCtrl.Param.Byte[0] = 5+3; // index // +3, weil bei HoTT V4 3 Bytes eingeschoben wurden |
481 | ToFlightCtrl.Param.Byte[1] = 2; // how many |
481 | ToFlightCtrl.Param.Byte[1] = 2; // how many |
482 | ToFlightCtrl.Param.Byte[2] = EarthMagneticField / (5 * 2); |
482 | ToFlightCtrl.Param.Byte[2] = EarthMagneticField / (5 * 2); |
483 | ToFlightCtrl.Param.Byte[3] = EarthMagneticInclination / 2; |
483 | ToFlightCtrl.Param.Byte[3] = EarthMagneticInclination / 2; |
484 | hott_index = 0; |
484 | hott_index = 0; |
485 | break; |
485 | break; |
486 | default: |
486 | default: |
487 | ToFlightCtrl.Param.Byte[0] = 255; |
487 | ToFlightCtrl.Param.Byte[0] = 255; |
488 | hott_index = 0; |
488 | hott_index = 0; |
489 | break; |
489 | break; |
490 | } |
490 | } |
491 | break; |
491 | break; |
492 | default: |
492 | default: |
493 | break; |
493 | break; |
494 | // 0 = 0,1 |
494 | // 0 = 0,1 |
495 | // 1 = 2,3 |
495 | // 1 = 2,3 |
496 | // 2 = 4,5 |
496 | // 2 = 4,5 |
497 | // 3 = 6,7 |
497 | // 3 = 6,7 |
498 | // 4 = 8,9 |
498 | // 4 = 8,9 |
499 | // 5 = 10,11 |
499 | // 5 = 10,11 |
500 | } |
500 | } |
501 | VIC_ITCmd(SSP0_ITLine, ENABLE); // enable SPI interrupt |
501 | VIC_ITCmd(SSP0_ITLine, ENABLE); // enable SPI interrupt |
502 | switch(FromFlightCtrl.Command) |
502 | switch(FromFlightCtrl.Command) |
503 | { |
503 | { |
504 | case SPI_FCCMD_USER: |
504 | case SPI_FCCMD_USER: |
505 | Parameter.User1 = FromFlightCtrl.Param.Byte[0]; |
505 | Parameter.User1 = FromFlightCtrl.Param.Byte[0]; |
506 | Parameter.User2 = FromFlightCtrl.Param.Byte[1]; |
506 | Parameter.User2 = FromFlightCtrl.Param.Byte[1]; |
507 | Parameter.User3 = FromFlightCtrl.Param.Byte[2]; |
507 | Parameter.User3 = FromFlightCtrl.Param.Byte[2]; |
508 | Parameter.User4 = FromFlightCtrl.Param.Byte[3]; |
508 | Parameter.User4 = FromFlightCtrl.Param.Byte[3]; |
509 | Parameter.User5 = FromFlightCtrl.Param.Byte[4]; |
509 | Parameter.User5 = FromFlightCtrl.Param.Byte[4]; |
510 | Parameter.User6 = FromFlightCtrl.Param.Byte[5]; |
510 | Parameter.User6 = FromFlightCtrl.Param.Byte[5]; |
511 | Parameter.User7 = FromFlightCtrl.Param.Byte[6]; |
511 | Parameter.User7 = FromFlightCtrl.Param.Byte[6]; |
512 | Parameter.User8 = FromFlightCtrl.Param.Byte[7]; |
512 | Parameter.User8 = FromFlightCtrl.Param.Byte[7]; |
513 | if(ClearFCStatusFlags) |
513 | if(ClearFCStatusFlags) |
514 | { |
514 | { |
515 | FC.StatusFlags = 0; |
515 | FC.StatusFlags = 0; |
516 | ClearFCStatusFlags = 0; |
516 | ClearFCStatusFlags = 0; |
517 | } |
517 | } |
518 | FC.StatusFlags |= FromFlightCtrl.Param.Byte[8]; |
518 | FC.StatusFlags |= FromFlightCtrl.Param.Byte[8]; |
519 | if(FC.StatusFlags & FC_STATUS_CALIBRATE && !FCCalibActive) |
519 | if(FC.StatusFlags & FC_STATUS_CALIBRATE && !FCCalibActive) |
520 | { |
520 | { |
521 | HeadFreeStartAngle = Compass_Heading * 10; |
521 | HeadFreeStartAngle = Compass_Heading * 10; |
522 | Compass_Init(); |
522 | Compass_Init(); |
523 | FCCalibActive = 10; |
523 | FCCalibActive = 10; |
524 | FC_is_Calibrated = 0; |
524 | FC_is_Calibrated = 0; |
525 | } |
525 | } |
526 | else |
526 | else |
527 | { |
527 | { |
528 | if(FCCalibActive) if(--FCCalibActive == 0) FC_is_Calibrated = 1; |
528 | if(FCCalibActive) if(--FCCalibActive == 0) FC_is_Calibrated = 1; |
529 | } |
529 | } |
530 | if(FC.StatusFlags & FC_STATUS_START) |
530 | if(FC.StatusFlags & FC_STATUS_START) |
531 | { |
531 | { |
532 | if(Compass_Heading != -1) HeadFreeStartAngle = Compass_Heading * 10; else |
532 | if(Compass_Heading != -1) HeadFreeStartAngle = Compass_Heading * 10; else |
533 | HeadFreeStartAngle = FromFlightCtrl.GyroHeading; |
533 | HeadFreeStartAngle = FromFlightCtrl.GyroHeading; |
534 | } |
534 | } |
535 | 535 | ||
536 | if((Parameter.ExtraConfig & CFG_TEACHABLE_CAREFREE)) |
536 | if((Parameter.ExtraConfig & CFG_TEACHABLE_CAREFREE)) |
537 | { |
537 | { |
538 | if(!(FC.StatusFlags2 & FC_STATUS2_CAREFREE)) // CF ist jetzt ausgeschaltet -> neue Richtung lernen |
538 | if(!(FC.StatusFlags2 & FC_STATUS2_CAREFREE)) // CF ist jetzt ausgeschaltet -> neue Richtung lernen |
539 | { |
539 | { |
540 | if((NaviData.HomePositionDeviation.Distance > 200) && (NCFlags & NC_FLAG_GPS_OK)) // nur bei ausreichender Distance -> 20m |
540 | if((NaviData.HomePositionDeviation.Distance > 200) && (NCFlags & NC_FLAG_GPS_OK)) // nur bei ausreichender Distance -> 20m |
541 | { |
541 | { |
542 | HeadFreeStartAngle = (10 * NaviData.HomePositionDeviation.Bearing + 1800 + 3600 - Parameter.OrientationAngle * 150) % 3600; // in 0.1° |
542 | HeadFreeStartAngle = (10 * NaviData.HomePositionDeviation.Bearing + 1800 + 3600 - Parameter.OrientationAngle * 150) % 3600; // in 0.1° |
543 | } |
543 | } |
544 | else // Ansonsten die aktuelle Richtung übernehmen |
544 | else // Ansonsten die aktuelle Richtung übernehmen |
545 | HeadFreeStartAngle = (3600 + FromFlightCtrl.GyroHeading /*+ Parameter.OrientationAngle * 150*/) % 3600; // in 0.1° |
545 | HeadFreeStartAngle = (3600 + FromFlightCtrl.GyroHeading /*+ Parameter.OrientationAngle * 150*/) % 3600; // in 0.1° |
546 | } |
546 | } |
547 | } |
547 | } |
548 | 548 | ||
549 | Parameter.ActiveSetting = FromFlightCtrl.Param.Byte[9]; |
549 | Parameter.ActiveSetting = FromFlightCtrl.Param.Byte[9]; |
550 | DebugOut.Analog[5] = FC.StatusFlags; |
550 | DebugOut.Analog[5] = FC.StatusFlags; |
551 | NaviData.FCStatusFlags = FC.StatusFlags; |
551 | NaviData.FCStatusFlags = FC.StatusFlags; |
552 | if(FC.StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) NaviData.FCStatusFlags &= ~FC_STATUS_FLY; |
552 | if(FC.StatusFlags2 & FC_STATUS2_WAIT_FOR_TAKEOFF) NaviData.FCStatusFlags &= ~FC_STATUS_FLY; |
553 | FC.StatusFlags2 = FromFlightCtrl.Param.Byte[11]; |
553 | FC.StatusFlags2 = FromFlightCtrl.Param.Byte[11]; |
554 | NaviData.FCStatusFlags2 = (NaviData.FCStatusFlags2 & (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE)) | (FC.StatusFlags2 & (0xff - (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE))); |
554 | NaviData.FCStatusFlags2 = (NaviData.FCStatusFlags2 & (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE)) | (FC.StatusFlags2 & (0xff - (FC_STATUS2_OUT1_ACTIVE | FC_STATUS2_OUT2_ACTIVE))); |
555 | 555 | ||
556 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT1_ACTIVE; |
556 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT1_ACTIVE; |
557 | else |
557 | else |
558 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT1_ACTIVE; |
558 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT1_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT1_ACTIVE; |
559 | 559 | ||
560 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT2_ACTIVE; |
560 | if((!(LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && (FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 |= FC_STATUS2_OUT2_ACTIVE; |
561 | else |
561 | else |
562 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT2_ACTIVE; |
562 | if(((LastTransmittedFCStatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) && !(FC.StatusFlags2 & FC_STATUS2_OUT2_ACTIVE)) NaviData.FCStatusFlags2 &= ~FC_STATUS2_OUT2_ACTIVE; |
563 | 563 | ||
564 | Logging_FCStatusFlags1 |= FC.StatusFlags; |
564 | Logging_FCStatusFlags1 |= FC.StatusFlags; |
565 | Logging_FCStatusFlags2 |= FC.StatusFlags2; |
565 | Logging_FCStatusFlags2 |= FC.StatusFlags2; |
566 | Parameter.ComingHomeAltitude = FromFlightCtrl.Param.Byte[10]; |
566 | Parameter.ComingHomeAltitude = FromFlightCtrl.Param.Byte[10]; |
567 | break; |
567 | break; |
568 | 568 | ||
569 | case SPI_FCCMD_BL_ACCU: |
569 | case SPI_FCCMD_BL_ACCU: |
570 | FC.BAT_Current = FromFlightCtrl.Param.Int[0]; |
570 | FC.BAT_Current = FromFlightCtrl.Param.Int[0]; |
571 | FC.BAT_UsedCapacity = FromFlightCtrl.Param.Int[1]; |
571 | FC.BAT_UsedCapacity = FromFlightCtrl.Param.Int[1]; |
572 | FC.BAT_Voltage = FromFlightCtrl.Param.Byte[4]; |
572 | FC.BAT_Voltage = FromFlightCtrl.Param.Byte[4]; |
573 | Parameter.NaviGpsModeControl = FromFlightCtrl.Param.Byte[5]; |
573 | Parameter.NaviGpsModeControl = FromFlightCtrl.Param.Byte[5]; |
574 | FromFC_VarioCharacter = FromFlightCtrl.Param.Byte[6]; |
574 | FromFC_VarioCharacter = FromFlightCtrl.Param.Byte[6]; |
575 | Motor[FromFlightCtrl.Param.Byte[7]].MaxPWM = FromFlightCtrl.Param.Byte[8]; |
575 | Motor[FromFlightCtrl.Param.Byte[7]].MaxPWM = FromFlightCtrl.Param.Byte[8]; |
576 | Motor[FromFlightCtrl.Param.Byte[7]].State = FromFlightCtrl.Param.Byte[9]; |
576 | Motor[FromFlightCtrl.Param.Byte[7]].State = FromFlightCtrl.Param.Byte[9]; |
577 | Motor[FromFlightCtrl.Param.Byte[7]].Temperature = FromFlightCtrl.Param.Byte[10]; |
577 | Motor[FromFlightCtrl.Param.Byte[7]].Temperature = FromFlightCtrl.Param.Byte[10]; |
578 | Motor[FromFlightCtrl.Param.Byte[7]].Current = FromFlightCtrl.Param.Byte[11]; |
578 | Motor[FromFlightCtrl.Param.Byte[7]].Current = FromFlightCtrl.Param.Byte[11]; |
579 | if(FromFC_VarioCharacter == '+' || FromFC_VarioCharacter == '-') // manual setpoint clears the NC-Parameter command |
579 | if(FromFC_VarioCharacter == '+' || FromFC_VarioCharacter == '-') // manual setpoint clears the NC-Parameter command |
580 | { |
580 | { |
581 | NCParams_ClearValue(NCPARAMS_ALTITUDE_RATE); |
581 | NCParams_ClearValue(NCPARAMS_ALTITUDE_RATE); |
582 | } |
582 | } |
583 | NaviData.UBat = FC.BAT_Voltage; |
583 | NaviData.UBat = FC.BAT_Voltage; |
584 | NaviData.Current = FC.BAT_Current; |
584 | NaviData.Current = FC.BAT_Current; |
585 | NaviData.UsedCapacity = FC.BAT_UsedCapacity; |
585 | NaviData.UsedCapacity = FC.BAT_UsedCapacity; |
586 | break; |
586 | break; |
587 | case SPI_FCCMD_PARAMETER1: |
587 | case SPI_FCCMD_PARAMETER1: |
588 | Parameter.LowVoltageWarning = FromFlightCtrl.Param.Byte[0]; |
588 | Parameter.LowVoltageWarning = FromFlightCtrl.Param.Byte[0]; |
589 | CHK_POTI_MM(Parameter.NaviGpsGain,FromFlightCtrl.Param.Byte[1],0,255); |
589 | CHK_POTI_MM(Parameter.NaviGpsGain,FromFlightCtrl.Param.Byte[1],0,255); |
590 | CHK_POTI_MM(Parameter.NaviGpsP,FromFlightCtrl.Param.Byte[2],0,255); |
590 | CHK_POTI_MM(Parameter.NaviGpsP,FromFlightCtrl.Param.Byte[2],0,255); |
591 | CHK_POTI_MM(Parameter.NaviGpsI,FromFlightCtrl.Param.Byte[3],0,255); |
591 | CHK_POTI_MM(Parameter.NaviGpsI,FromFlightCtrl.Param.Byte[3],0,255); |
592 | CHK_POTI_MM(Parameter.NaviGpsD,FromFlightCtrl.Param.Byte[4],0,255); |
592 | CHK_POTI_MM(Parameter.NaviGpsD,FromFlightCtrl.Param.Byte[4],0,255); |
593 | CHK_POTI_MM(Parameter.NaviGpsACC,FromFlightCtrl.Param.Byte[5],0,255); |
593 | CHK_POTI_MM(Parameter.NaviGpsACC,FromFlightCtrl.Param.Byte[5],0,255); |
594 | Parameter.NaviGpsMinSat = FromFlightCtrl.Param.Byte[6]; |
594 | Parameter.NaviGpsMinSat = FromFlightCtrl.Param.Byte[6]; |
595 | Parameter.NaviStickThreshold = FromFlightCtrl.Param.Byte[7]; |
595 | Parameter.NaviStickThreshold = FromFlightCtrl.Param.Byte[7]; |
596 | CHK_POTI_MM(Parameter.NaviOperatingRadius,FromFlightCtrl.Param.Byte[8],0,255); |
596 | CHK_POTI_MM(Parameter.NaviOperatingRadius,FromFlightCtrl.Param.Byte[8],0,255); |
597 | CHK_POTI_MM(Parameter.NaviWindCorrection,FromFlightCtrl.Param.Byte[9],0,255); |
597 | CHK_POTI_MM(Parameter.NaviWindCorrection,FromFlightCtrl.Param.Byte[9],0,255); |
598 | CHK_POTI_MM(Parameter.NaviAccCompensation,FromFlightCtrl.Param.Byte[10],0,255); |
598 | CHK_POTI_MM(Parameter.NaviAccCompensation,FromFlightCtrl.Param.Byte[10],0,255); |
599 | CHK_POTI_MM(Parameter.NaviAngleLimitation,FromFlightCtrl.Param.Byte[11],0,255); |
599 | CHK_POTI_MM(Parameter.NaviAngleLimitation,FromFlightCtrl.Param.Byte[11],0,255); |
600 | break; |
600 | break; |
601 | case SPI_FCCMD_PARAMETER2: |
601 | case SPI_FCCMD_PARAMETER2: |
602 | CHK_POTI_MM(Parameter.NaviOut1Parameter,FromFlightCtrl.Param.Byte[0],0,255); |
602 | CHK_POTI_MM(Parameter.NaviOut1Parameter,FromFlightCtrl.Param.Byte[0],0,255); |
603 | if(FromFlightCtrl.Param.Byte[1]) FC.FromFC_SpeakHoTT = FromFlightCtrl.Param.Byte[1]; // will be cleared in the SD-Logging |
603 | if(FromFlightCtrl.Param.Byte[1]) FC.FromFC_SpeakHoTT = FromFlightCtrl.Param.Byte[1]; // will be cleared in the SD-Logging |
604 | Parameter.FromFC_LandingSpeed = FromFlightCtrl.Param.Byte[2]; |
604 | Parameter.FromFC_LandingSpeed = FromFlightCtrl.Param.Byte[2]; |
605 | break; |
605 | break; |
606 | case SPI_FCCMD_STICK: |
606 | case SPI_FCCMD_STICK: |
607 | FC.StickGas = FromFlightCtrl.Param.sByte[0]; |
607 | FC.StickGas = FromFlightCtrl.Param.sByte[0]; |
608 | FC.StickYaw = FromFlightCtrl.Param.sByte[1]; |
608 | FC.StickYaw = FromFlightCtrl.Param.sByte[1]; |
609 | FC.StickRoll = FromFlightCtrl.Param.sByte[2]; |
609 | FC.StickRoll = FromFlightCtrl.Param.sByte[2]; |
610 | FC.StickNick = FromFlightCtrl.Param.sByte[3]; |
610 | FC.StickNick = FromFlightCtrl.Param.sByte[3]; |
611 | FC.Poti[0] = FromFlightCtrl.Param.Byte[4]; |
611 | FC.Poti[0] = FromFlightCtrl.Param.Byte[4]; |
612 | FC.Poti[1] = FromFlightCtrl.Param.Byte[5]; |
612 | FC.Poti[1] = FromFlightCtrl.Param.Byte[5]; |
613 | FC.Poti[2] = FromFlightCtrl.Param.Byte[6]; |
613 | FC.Poti[2] = FromFlightCtrl.Param.Byte[6]; |
614 | FC.Poti[3] = FromFlightCtrl.Param.Byte[7]; |
614 | FC.Poti[3] = FromFlightCtrl.Param.Byte[7]; |
615 | FC.Poti[4] = FromFlightCtrl.Param.Byte[8]; |
615 | FC.Poti[4] = FromFlightCtrl.Param.Byte[8]; |
616 | FC.Poti[5] = FromFlightCtrl.Param.Byte[9]; |
616 | FC.Poti[5] = FromFlightCtrl.Param.Byte[9]; |
617 | FC.Poti[6] = FromFlightCtrl.Param.Byte[10]; |
617 | FC.Poti[6] = FromFlightCtrl.Param.Byte[10]; |
618 | FC.Poti[7] = FromFlightCtrl.Param.Byte[11]; |
618 | FC.Poti[7] = FromFlightCtrl.Param.Byte[11]; |
619 | CHK_POTI_MM(WaypointAcceleration,WaypointAccelerationSetting,0,255); // that could be a Poti-Value |
619 | CHK_POTI_MM(WaypointAcceleration,WaypointAccelerationSetting,0,255); // that could be a Poti-Value |
620 | break; |
620 | break; |
621 | 621 | ||
622 | case SPI_FCCMD_MISC: |
622 | case SPI_FCCMD_MISC: |
623 | if(CompassCalState != FromFlightCtrl.Param.Byte[0]) |
623 | if(CompassCalState != FromFlightCtrl.Param.Byte[0]) |
624 | { // put only new CompassCalState into queue to send via I2C |
624 | { // put only new CompassCalState into queue to send via I2C |
625 | // if(FromFlightCtrl.Param.Byte[0] == CompassCalState+1 || FromFlightCtrl.Param.Byte[0] == 0) |
625 | // if(FromFlightCtrl.Param.Byte[0] == CompassCalState+1 || FromFlightCtrl.Param.Byte[0] == 0) |
626 | { |
626 | { |
627 | CompassCalState = FromFlightCtrl.Param.Byte[0]; |
627 | CompassCalState = FromFlightCtrl.Param.Byte[0]; |
628 | Compass_SetCalState(CompassCalState); |
628 | Compass_SetCalState(CompassCalState); |
629 | } |
629 | } |
630 | // else CompassCalState = 0; |
630 | // else CompassCalState = 0; |
631 | } |
631 | } |
632 | Parameter.NaviPH_LoginTime = FromFlightCtrl.Param.Byte[1]; |
632 | Parameter.NaviPH_LoginTime = FromFlightCtrl.Param.Byte[1]; |
633 | NaviData.Variometer = (NaviData.Variometer + 2 * (FromFlightCtrl.Param.sInt[1] - NaviData.Altimeter)) / 2; // provisorisch |
633 | NaviData.Variometer = (NaviData.Variometer + 2 * (FromFlightCtrl.Param.sInt[1] - NaviData.Altimeter)) / 2; // provisorisch |
634 | NaviData.Altimeter = FromFlightCtrl.Param.sInt[1]; // in 5cm |
634 | NaviData.Altimeter = FromFlightCtrl.Param.sInt[1]; // in 5cm |
635 | NaviData.SetpointAltitude = FromFlightCtrl.Param.sInt[2]; // in 5cm |
635 | NaviData.SetpointAltitude = FromFlightCtrl.Param.sInt[2]; // in 5cm |
636 | CHK_POTI_MM(Parameter.NaviGpsPLimit,FromFlightCtrl.Param.Byte[6],0,255); |
636 | CHK_POTI_MM(Parameter.NaviGpsPLimit,FromFlightCtrl.Param.Byte[6],0,255); |
637 | CHK_POTI_MM(Parameter.NaviGpsILimit,FromFlightCtrl.Param.Byte[7],0,255); |
637 | CHK_POTI_MM(Parameter.NaviGpsILimit,FromFlightCtrl.Param.Byte[7],0,255); |
638 | CHK_POTI_MM(Parameter.NaviGpsDLimit,FromFlightCtrl.Param.Byte[8],0,255); |
638 | CHK_POTI_MM(Parameter.NaviGpsDLimit,FromFlightCtrl.Param.Byte[8],0,255); |
639 | FC.RC_Quality = FromFlightCtrl.Param.Byte[9]; |
639 | FC.RC_Quality = FromFlightCtrl.Param.Byte[9]; |
640 | NaviData.RC_Quality = FC.RC_Quality; |
640 | NaviData.RC_Quality = FC.RC_Quality; |
641 | //FromFlightCtrl.Param.Byte[10]; |
641 | //FromFlightCtrl.Param.Byte[10]; |
642 | 642 | ||
643 | // FC.RC_RSSI = FromFlightCtrl.Param.Byte[10]; |
643 | // FC.RC_RSSI = FromFlightCtrl.Param.Byte[10]; |
644 | // if(!FC.RC_RSSI) NaviData.RC_Quality = FC.RC_Quality; else NaviData.RC_Quality = FC.RC_RSSI; |
644 | // if(!FC.RC_RSSI) NaviData.RC_Quality = FC.RC_Quality; else NaviData.RC_Quality = FC.RC_RSSI; |
645 | // NaviData.RC_RSSI = FC.RC_RSSI; |
645 | // NaviData.RC_RSSI = FC.RC_RSSI; |
646 | NaviData.Gas = (FC.BAT_Voltage * (u32) FromFlightCtrl.Param.Byte[11]) / (u32) Parameter.LowVoltageWarning; |
646 | NaviData.Gas = (FC.BAT_Voltage * (u32) FromFlightCtrl.Param.Byte[11]) / (u32) Parameter.LowVoltageWarning; |
647 | break; |
647 | break; |
648 | 648 | ||
649 | case SPI_FCCMD_SERVOS: |
649 | case SPI_FCCMD_SERVOS: |
650 | ServoParams.Refresh = FromFlightCtrl.Param.Byte[0]; |
650 | ServoParams.Refresh = FromFlightCtrl.Param.Byte[0]; |
651 | ServoParams.CompInvert = FromFlightCtrl.Param.Byte[1]; |
651 | ServoParams.CompInvert = FromFlightCtrl.Param.Byte[1]; |
652 | ServoParams.NickControl = FromFlightCtrl.Param.Byte[2]; |
652 | ServoParams.NickControl = FromFlightCtrl.Param.Byte[2]; |
653 | ServoParams.NickComp = FromFlightCtrl.Param.Byte[3]; |
653 | ServoParams.NickComp = FromFlightCtrl.Param.Byte[3]; |
654 | ServoParams.NickMin = FromFlightCtrl.Param.Byte[4]; |
654 | ServoParams.NickMin = FromFlightCtrl.Param.Byte[4]; |
655 | ServoParams.NickMax = FromFlightCtrl.Param.Byte[5]; |
655 | ServoParams.NickMax = FromFlightCtrl.Param.Byte[5]; |
656 | ServoParams.RollControl = FromFlightCtrl.Param.Byte[6]; |
656 | ServoParams.RollControl = FromFlightCtrl.Param.Byte[6]; |
657 | ServoParams.RollComp = FromFlightCtrl.Param.Byte[7]; |
657 | ServoParams.RollComp = FromFlightCtrl.Param.Byte[7]; |
658 | ServoParams.RollMin = FromFlightCtrl.Param.Byte[8]; |
658 | ServoParams.RollMin = FromFlightCtrl.Param.Byte[8]; |
659 | ServoParams.RollMax = FromFlightCtrl.Param.Byte[9]; |
659 | ServoParams.RollMax = FromFlightCtrl.Param.Byte[9]; |
660 | BL_MinOfMaxPWM = FromFlightCtrl.Param.Byte[10]; |
660 | BL_MinOfMaxPWM = FromFlightCtrl.Param.Byte[10]; |
661 | FC_I2C_ErrorConter = FromFlightCtrl.Param.Byte[11]; |
661 | FC_I2C_ErrorConter = FromFlightCtrl.Param.Byte[11]; |
662 | break; |
662 | break; |
663 | 663 | ||
664 | case SPI_FCCMD_VERSION: |
664 | case SPI_FCCMD_VERSION: |
665 | FC_Version.Major = FromFlightCtrl.Param.Byte[0]; |
665 | FC_Version.Major = FromFlightCtrl.Param.Byte[0]; |
666 | FC_Version.Minor = FromFlightCtrl.Param.Byte[1]; |
666 | FC_Version.Minor = FromFlightCtrl.Param.Byte[1]; |
667 | FC_Version.Patch = FromFlightCtrl.Param.Byte[2]; |
667 | FC_Version.Patch = FromFlightCtrl.Param.Byte[2]; |
668 | FC_Version.Compatible = FromFlightCtrl.Param.Byte[3]; |
668 | FC_Version.Compatible = FromFlightCtrl.Param.Byte[3]; |
669 | FC_Version.Hardware = FromFlightCtrl.Param.Byte[4]; |
669 | FC_Version.Hardware = FromFlightCtrl.Param.Byte[4]; |
670 | FC.Error[0] |= FromFlightCtrl.Param.Byte[5]; |
670 | FC.Error[0] |= FromFlightCtrl.Param.Byte[5]; |
671 | FC.Error[1] |= FromFlightCtrl.Param.Byte[6]; |
671 | FC.Error[1] |= FromFlightCtrl.Param.Byte[6]; |
672 | FC.Error[2] |= FromFlightCtrl.Param.Byte[7]; |
672 | // frei FC.Error[2] |= FromFlightCtrl.Param.Byte[7]; |
673 | Parameter.GlobalConfig = FromFlightCtrl.Param.Byte[8]; |
673 | Parameter.GlobalConfig = FromFlightCtrl.Param.Byte[8]; |
674 | Parameter.ExtraConfig = FromFlightCtrl.Param.Byte[9]; |
674 | Parameter.ExtraConfig = FromFlightCtrl.Param.Byte[9]; |
675 | Parameter.OrientationAngle = FromFlightCtrl.Param.Byte[10]; |
675 | Parameter.OrientationAngle = FromFlightCtrl.Param.Byte[10]; |
676 | Parameter.GlobalConfig3 = FromFlightCtrl.Param.Byte[11]; |
676 | Parameter.GlobalConfig3 = FromFlightCtrl.Param.Byte[11]; |
677 | DebugOut.StatusGreen |= AMPEL_FC; // status of FC Present |
677 | DebugOut.StatusGreen |= AMPEL_FC; // status of FC Present |
678 | DebugOut.StatusGreen |= AMPEL_BL; // status of BL Present |
678 | DebugOut.StatusGreen |= AMPEL_BL; // status of BL Present |
679 | if(FC.Error[0] || FC.Error[1] || FC.Error[2] || FC.Error[3] || FC.Error[4]) DebugOut.StatusRed |= AMPEL_FC; |
679 | if(FC.Error[0] || FC.Error[1] /* || FC.Error[2] || FC.Error[3] || FC.Error[4]*/) DebugOut.StatusRed |= AMPEL_FC; |
680 | else DebugOut.StatusRed &= ~AMPEL_FC; |
680 | else DebugOut.StatusRed &= ~AMPEL_FC; |
681 | break; |
681 | break; |
682 | default: |
682 | default: |
683 | break; |
683 | break; |
684 | } |
684 | } |
685 | 685 | ||
686 | DebugOut.Analog[0] = FromFlightCtrl.AngleNick; |
686 | DebugOut.Analog[0] = FromFlightCtrl.AngleNick; |
687 | DebugOut.Analog[1] = FromFlightCtrl.AngleRoll; |
687 | DebugOut.Analog[1] = FromFlightCtrl.AngleRoll; |
688 | DebugOut.Analog[2] = FromFlightCtrl.AccNick; |
688 | DebugOut.Analog[2] = FromFlightCtrl.AccNick; |
689 | DebugOut.Analog[3] = FromFlightCtrl.AccRoll; |
689 | DebugOut.Analog[3] = FromFlightCtrl.AccRoll; |
690 | DebugOut.Analog[11] = FromFlightCtrl.GyroHeading/10;// in deg |
690 | DebugOut.Analog[11] = FromFlightCtrl.GyroHeading/10;// in deg |
691 | Data3D.AngleNick = FromFlightCtrl.AngleNick; // in 0.1 deg |
691 | Data3D.AngleNick = FromFlightCtrl.AngleNick; // in 0.1 deg |
692 | Data3D.AngleRoll = FromFlightCtrl.AngleRoll; // in 0.1 deg |
692 | Data3D.AngleRoll = FromFlightCtrl.AngleRoll; // in 0.1 deg |
693 | Data3D.Heading = FromFlightCtrl.GyroHeading; // in 0.1 deg |
693 | Data3D.Heading = FromFlightCtrl.GyroHeading; // in 0.1 deg |
694 | // every time we got new data from the FC via SPI call the navigation routine |
694 | // every time we got new data from the FC via SPI call the navigation routine |
695 | // and update GPSStick that are returned to FC |
695 | // and update GPSStick that are returned to FC |
696 | SPI_RxBuffer_Request = 0; |
696 | SPI_RxBuffer_Request = 0; |
697 | GPS_Navigation(&GPSData, &(ToFlightCtrl.GPSStick)); |
697 | GPS_Navigation(&GPSData, &(ToFlightCtrl.GPSStick)); |
698 | ClearFCStatusFlags = 1; |
698 | ClearFCStatusFlags = 1; |
699 | if(counter) |
699 | if(counter) |
700 | { |
700 | { |
701 | counter--; // count down to enable servo |
701 | counter--; // count down to enable servo |
702 | if(!counter) TIMER2_Init(); // enable Servo Output |
702 | if(!counter) TIMER2_Init(); // enable Servo Output |
703 | } |
703 | } |
704 | timeout = SetDelay(80); // 80 ms, new data are send every 20 ms |
704 | timeout = SetDelay(80); // 80 ms, new data are send every 20 ms |
705 | 705 | ||
706 | } // EOF if(SPI_RxBuffer_Request) |
706 | } // EOF if(SPI_RxBuffer_Request) |
707 | else // no new SPI data |
707 | else // no new SPI data |
708 | { |
708 | { |
709 | if(CheckDelay(timeout) && (counter == 0)) |
709 | if(CheckDelay(timeout) && (counter == 0)) |
710 | { |
710 | { |
711 | TIMER2_Deinit(); // disable Servo Output |
711 | TIMER2_Deinit(); // disable Servo Output |
712 | counter = 50; // reset counter for enabling Servo Output |
712 | counter = 50; // reset counter for enabling Servo Output |
713 | } |
713 | } |
714 | } |
714 | } |
715 | } |
715 | } |
716 | 716 | ||
717 | //------------------------------------------------------ |
717 | //------------------------------------------------------ |
718 | void SPI0_GetFlightCtrlVersion(void) |
718 | void SPI0_GetFlightCtrlVersion(void) |
719 | { |
719 | { |
720 | u32 timeout; |
720 | u32 timeout; |
721 | u8 repeat; |
721 | u8 repeat; |
722 | u8 msg[64]; |
722 | u8 msg[64]; |
723 | 723 | ||
724 | UART1_PutString("\r\n Looking for FlightControl"); |
724 | UART1_PutString("\r\n Looking for FlightControl"); |
725 | FC_Version.Major = 0xFF; |
725 | FC_Version.Major = 0xFF; |
726 | FC_Version.Minor = 0xFF; |
726 | FC_Version.Minor = 0xFF; |
727 | FC_Version.Patch = 0xFF; |
727 | FC_Version.Patch = 0xFF; |
728 | FC_Version.Compatible = 0xFF; |
728 | FC_Version.Compatible = 0xFF; |
729 | 729 | ||
730 | // polling FC version info |
730 | // polling FC version info |
731 | repeat = 0; |
731 | repeat = 0; |
732 | do |
732 | do |
733 | { |
733 | { |
734 | timeout = SetDelay(250); |
734 | timeout = SetDelay(250); |
735 | do |
735 | do |
736 | { |
736 | { |
737 | SPI0_UpdateBuffer(); |
737 | SPI0_UpdateBuffer(); |
738 | if (FC_Version.Major != 0xFF) break; |
738 | if (FC_Version.Major != 0xFF) break; |
739 | }while (!CheckDelay(timeout)); |
739 | }while (!CheckDelay(timeout)); |
740 | UART1_PutString("."); |
740 | UART1_PutString("."); |
741 | repeat++; |
741 | repeat++; |
742 | FCCalibActive = 1; |
742 | FCCalibActive = 1; |
743 | }while((FC_Version.Major == 0xFF) && (repeat < 40)); // 40*250ms = 10s |
743 | }while((FC_Version.Major == 0xFF) && (repeat < 40)); // 40*250ms = 10s |
744 | // if we got it |
744 | // if we got it |
745 | if (FC_Version.Major != 0xFF) |
745 | if (FC_Version.Major != 0xFF) |
746 | { |
746 | { |
747 | 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); |
747 | 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); |
748 | UART1_PutString(msg); |
748 | UART1_PutString(msg); |
749 | } |
749 | } |
750 | else UART1_PutString("\n\r not found!"); |
750 | else UART1_PutString("\n\r not found!"); |
751 | } |
751 | } |
752 | 752 | ||
753 | 753 | ||
754 | 754 |