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1 | /*#######################################################################################*/ |
1 | /*#######################################################################################*/ |
2 | /*#######################################################################################*/ |
2 | /*#######################################################################################*/ |
3 | 3 | ||
4 | // IMPORTANT NOTE: |
4 | // IMPORTANT NOTE: |
5 | 5 | ||
6 | // This is only a dummy implementation for errorfree compiling of the NaviCtrl sources. |
6 | // This is only a dummy implementation for errorfree compiling of the NaviCtrl sources. |
7 | 7 | ||
8 | // The GPS navigation routines are NOT included ! |
8 | // The GPS navigation routines are NOT included ! |
9 | 9 | ||
10 | /*#######################################################################################*/ |
10 | /*#######################################################################################*/ |
11 | /*#######################################################################################*/ |
11 | /*#######################################################################################*/ |
12 | /* !!! THIS IS NOT FREE SOFTWARE !!! */ |
12 | /* !!! THIS IS NOT FREE SOFTWARE !!! */ |
13 | /*#######################################################################################*/ |
13 | /*#######################################################################################*/ |
14 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
14 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
15 | // + Copyright (c) 2008 Ingo Busker, Holger Buss |
15 | // + Copyright (c) 2008 Ingo Busker, Holger Buss |
16 | // + Nur für den privaten Gebrauch |
16 | // + Nur für den privaten Gebrauch |
17 | // + FOR NON COMMERCIAL USE ONLY |
17 | // + FOR NON COMMERCIAL USE ONLY |
18 | // + www.MikroKopter.com |
18 | // + www.MikroKopter.com |
19 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
19 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
20 | // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
20 | // + Es gilt für das gesamte Projekt (Hardware, Software, Binärfiles, Sourcecode und Dokumentation), |
21 | // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
21 | // + dass eine Nutzung (auch auszugsweise) nur für den privaten (nicht-kommerziellen) Gebrauch zulässig ist. |
22 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
22 | // + Sollten direkte oder indirekte kommerzielle Absichten verfolgt werden, ist mit uns (info@mikrokopter.de) Kontakt |
23 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
23 | // + bzgl. der Nutzungsbedingungen aufzunehmen. |
24 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
24 | // + Eine kommerzielle Nutzung ist z.B.Verkauf von MikroKoptern, Bestückung und Verkauf von Platinen oder Bausätzen, |
25 | // + Verkauf von Luftbildaufnahmen, usw. |
25 | // + Verkauf von Luftbildaufnahmen, usw. |
26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
26 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
27 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
27 | // + Werden Teile des Quellcodes (mit oder ohne Modifikation) weiterverwendet oder veröffentlicht, |
28 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
28 | // + unterliegen sie auch diesen Nutzungsbedingungen und diese Nutzungsbedingungen incl. Copyright müssen dann beiliegen |
29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
29 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
30 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
30 | // + Sollte die Software (auch auszugesweise) oder sonstige Informationen des MikroKopter-Projekts |
31 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
31 | // + auf anderen Webseiten oder sonstigen Medien veröffentlicht werden, muss unsere Webseite "http://www.mikrokopter.de" |
32 | // + eindeutig als Ursprung verlinkt werden |
32 | // + eindeutig als Ursprung verlinkt werden |
33 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
33 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
34 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
34 | // + Keine Gewähr auf Fehlerfreiheit, Vollständigkeit oder Funktion |
35 | // + Benutzung auf eigene Gefahr |
35 | // + Benutzung auf eigene Gefahr |
36 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
36 | // + Wir übernehmen keinerlei Haftung für direkte oder indirekte Personen- oder Sachschäden |
37 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
37 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
38 | // + Die PORTIERUNG der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
38 | // + Die PORTIERUNG der Software (oder Teile davon) auf andere Systeme (ausser der Hardware von www.mikrokopter.de) ist nur |
39 | // + mit unserer Zustimmung zulässig |
39 | // + mit unserer Zustimmung zulässig |
40 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
40 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
41 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
41 | // + Die Funktion printf_P() unterliegt ihrer eigenen Lizenz und ist hiervon nicht betroffen |
42 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
42 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
43 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
43 | // + Redistributions of source code (with or without modifications) must retain the above copyright notice, |
44 | // + this list of conditions and the following disclaimer. |
44 | // + this list of conditions and the following disclaimer. |
45 | // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
45 | // + * Neither the name of the copyright holders nor the names of contributors may be used to endorse or promote products derived |
46 | // + from this software without specific prior written permission. |
46 | // + from this software without specific prior written permission. |
47 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permitted |
47 | // + * The use of this project (hardware, software, binary files, sources and documentation) is only permitted |
48 | // + for non-commercial use (directly or indirectly) |
48 | // + for non-commercial use (directly or indirectly) |
49 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
49 | // + Commercial use (for excample: selling of MikroKopters, selling of PCBs, assembly, ...) is only permitted |
50 | // + with our written permission |
50 | // + with our written permission |
51 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
51 | // + * If sources or documentations are redistributet on other webpages, out webpage (http://www.MikroKopter.de) must be |
52 | // + clearly linked as origin |
52 | // + clearly linked as origin |
53 | // + * PORTING this software (or part of it) to systems (other than hardware from www.mikrokopter.de) is NOT allowed |
53 | // + * PORTING this software (or part of it) to systems (other than hardware from www.mikrokopter.de) is NOT allowed |
54 | // |
54 | // |
55 | // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
55 | // + THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" |
56 | // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
56 | // + AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE |
57 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
57 | // + IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE |
58 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
58 | // + ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE |
59 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
59 | // + LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR |
60 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
60 | // + CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF |
61 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
61 | // + SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS |
62 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
62 | // + INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN |
63 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
63 | // + CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) |
64 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
64 | // + ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE |
65 | // + POSSIBILITY OF SUCH DAMAGE. |
65 | // + POSSIBILITY OF SUCH DAMAGE. |
66 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
66 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
67 | #include <stdio.h> |
67 | #include <stdio.h> |
68 | #include <stdlib.h> |
68 | #include <stdlib.h> |
69 | #include <math.h> |
69 | #include <math.h> |
70 | #include "91x_lib.h" |
70 | #include "91x_lib.h" |
71 | #include "main.h" |
71 | #include "main.h" |
72 | #include "uart1.h" |
72 | #include "uart1.h" |
73 | #include "GPS.h" |
73 | #include "GPS.h" |
74 | #include "timer.h" |
74 | #include "timer.h" |
75 | #include "spi_slave.h" |
75 | #include "spi_slave.h" |
76 | #include "waypoints.h" |
76 | #include "waypoints.h" |
77 | #include "i2c.h" |
77 | #include "i2c.h" |
78 | 78 | ||
79 | 79 | ||
80 | #define M_PI_180 (M_PI / 180.0f) |
80 | #define M_PI_180 (M_PI / 180.0f) |
81 | #define GPS_UPDATETIME_MS 200 // 200ms is 5 Hz |
81 | #define GPS_UPDATETIME_MS 200 // 200ms is 5 Hz |
82 | typedef enum |
82 | typedef enum |
83 | { |
83 | { |
84 | GPS_FLIGHT_MODE_UNDEF, |
84 | GPS_FLIGHT_MODE_UNDEF, |
85 | GPS_FLIGHT_MODE_FREE, |
85 | GPS_FLIGHT_MODE_FREE, |
86 | GPS_FLIGHT_MODE_AID, |
86 | GPS_FLIGHT_MODE_AID, |
87 | GPS_FLIGHT_MODE_WAYPOINT |
87 | GPS_FLIGHT_MODE_WAYPOINT |
88 | } GPS_FlightMode_t; |
88 | } GPS_FlightMode_t; |
89 | 89 | ||
90 | typedef struct |
90 | typedef struct |
91 | { |
91 | { |
92 | float Gain; |
92 | float Gain; |
93 | float P; |
93 | float P; |
94 | float I; |
94 | float I; |
95 | float D; |
95 | float D; |
96 | float A; |
96 | float A; |
97 | float ACC; |
97 | float ACC; |
98 | u32 P_Limit; |
98 | s32 P_Limit; |
99 | u32 I_Limit; |
99 | s32 I_Limit; |
100 | u32 D_Limit; |
100 | s32 D_Limit; |
101 | u32 PID_Limit; |
101 | s32 PID_Limit; |
102 | u32 BrakingDuration; |
102 | u32 BrakingDuration; |
103 | u8 MinSat; |
103 | u8 MinSat; |
104 | s8 StickThreshold; |
104 | s8 StickThreshold; |
105 | float WindCorrection; |
105 | float WindCorrection; |
106 | float SpeedCompensation; |
106 | float SpeedCompensation; |
107 | u32 OperatingRadius; |
107 | s32 OperatingRadius; |
108 | GPS_FlightMode_t FlightMode; |
108 | GPS_FlightMode_t FlightMode; |
109 | } __attribute__((packed)) GPS_Parameter_t; |
109 | } __attribute__((packed)) GPS_Parameter_t; |
110 | 110 | ||
111 | typedef struct |
111 | typedef struct |
112 | { |
112 | { |
113 | u8 Status; // invalid, newdata, processed |
113 | u8 Status; // invalid, newdata, processed |
114 | s32 North; // in cm |
114 | s32 North; // in cm |
115 | s32 East; // in cm |
115 | s32 East; // in cm |
116 | s32 Bearing; // in deg |
116 | s32 Bearing; // in deg |
117 | u32 Distance; // in cm |
117 | s32 Distance; // in cm |
118 | } __attribute__((packed)) GPS_Deviation_t; |
118 | } __attribute__((packed)) GPS_Deviation_t; |
119 | GPS_Deviation_t CurrentTargetDeviation; // Deviation from Target |
119 | GPS_Deviation_t CurrentTargetDeviation; // Deviation from Target |
120 | GPS_Deviation_t CurrentHomeDeviation; // Deviation from Home |
120 | GPS_Deviation_t CurrentHomeDeviation; // Deviation from Home |
121 | GPS_Deviation_t TargetHomeDeviation; // Deviation from Target to Home |
121 | GPS_Deviation_t TargetHomeDeviation; // Deviation from Target to Home |
122 | 122 | ||
123 | GPS_Stick_t GPS_Stick; |
123 | GPS_Stick_t GPS_Stick; |
124 | GPS_Parameter_t GPS_Parameter; |
124 | GPS_Parameter_t GPS_Parameter; |
125 | 125 | ||
126 | // the gps reference positions |
126 | // the gps reference positions |
127 | GPS_Pos_t GPS_HoldPosition = {0,0,0, INVALID}; // the hold position |
127 | GPS_Pos_t GPS_HoldPosition = {0,0,0, INVALID}; // the hold position |
128 | GPS_Pos_t GPS_HomePosition = {0,0,0, INVALID}; // the home position |
128 | GPS_Pos_t GPS_HomePosition = {0,0,0, INVALID}; // the home position |
129 | GPS_Pos_t * GPS_pTargetPosition = NULL; // pointer to the actual target position |
129 | GPS_Pos_t * GPS_pTargetPosition = NULL; // pointer to the actual target position |
130 | u32 GPS_TargetRadius = 0; // catch radius for target area |
130 | u32 GPS_TargetRadius = 0; // catch radius for target area |
131 | Waypoint_t* GPS_pWaypoint = NULL; // pointer to the actual waypoint |
131 | Waypoint_t* GPS_pWaypoint = NULL; // pointer to the actual waypoint |
132 | 132 | ||
133 | //------------------------------------------------------------- |
133 | //------------------------------------------------------------- |
134 | // Update GPSParamter |
134 | // Update GPSParamter |
135 | void GPS_UpdateParameter(void) |
135 | void GPS_UpdateParameter(void) |
136 | { |
136 | { |
137 | static GPS_FlightMode_t FlightMode_Old = GPS_FLIGHT_MODE_UNDEF; |
137 | static GPS_FlightMode_t FlightMode_Old = GPS_FLIGHT_MODE_UNDEF; |
138 | // in case of bad receiving conditions |
138 | // in case of bad receiving conditions |
139 | if(FC.RC_Quality < 100) |
139 | if(FC.RC_Quality < 100) |
140 | { // set fixed parameter |
140 | { // set fixed parameter |
141 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_WAYPOINT; |
141 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_WAYPOINT; |
142 | GPS_Parameter.Gain = (float) 100; |
142 | GPS_Parameter.Gain = (float) 100; |
143 | GPS_Parameter.P = (float) 90; |
143 | GPS_Parameter.P = (float) 90; |
144 | GPS_Parameter.I = (float) 90; |
144 | GPS_Parameter.I = (float) 90; |
145 | GPS_Parameter.D = (float) 90; |
145 | GPS_Parameter.D = (float) 90; |
146 | GPS_Parameter.A = (float) 90; |
146 | GPS_Parameter.A = (float) 90; |
147 | GPS_Parameter.ACC = (float) 0; |
147 | GPS_Parameter.ACC = (float) 0; |
148 | GPS_Parameter.P_Limit = 90; |
148 | GPS_Parameter.P_Limit = 90; |
149 | GPS_Parameter.I_Limit = 90; |
149 | GPS_Parameter.I_Limit = 90; |
150 | GPS_Parameter.D_Limit = 90; |
150 | GPS_Parameter.D_Limit = 90; |
151 | GPS_Parameter.PID_Limit = 200; |
151 | GPS_Parameter.PID_Limit = 200; |
152 | GPS_Parameter.BrakingDuration = 0; |
152 | GPS_Parameter.BrakingDuration = 0; |
153 | GPS_Parameter.SpeedCompensation = (float) 30; |
153 | GPS_Parameter.SpeedCompensation = (float) 30; |
154 | GPS_Parameter.MinSat = 6; |
154 | GPS_Parameter.MinSat = 6; |
155 | GPS_Parameter.StickThreshold = 8; |
155 | GPS_Parameter.StickThreshold = 8; |
156 | GPS_Parameter.WindCorrection = 0.0; |
156 | GPS_Parameter.WindCorrection = 0.0; |
157 | GPS_Parameter.OperatingRadius = 0; // forces the aircraft to fly to home positon |
157 | GPS_Parameter.OperatingRadius = 0; // forces the aircraft to fly to home positon |
158 | 158 | ||
159 | } |
159 | } |
160 | else |
160 | else |
161 | { |
161 | { |
162 | // update parameter from FC |
162 | // update parameter from FC |
163 | if(StopNavigation) GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_FREE; |
163 | if(StopNavigation) GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_FREE; |
164 | else |
164 | else |
165 | { |
165 | { |
166 | if(Parameter.NaviGpsModeControl < 50) |
166 | if(Parameter.NaviGpsModeControl < 50) |
167 | { |
167 | { |
168 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_FREE; |
168 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_FREE; |
169 | NCFlags &= ~(NC_FLAG_PH | NC_FLAG_CH); |
169 | NCFlags &= ~(NC_FLAG_PH | NC_FLAG_CH); |
170 | NCFlags |= NC_FLAG_FREE; |
170 | NCFlags |= NC_FLAG_FREE; |
171 | } |
171 | } |
172 | else if(Parameter.NaviGpsModeControl < 180) |
172 | else if(Parameter.NaviGpsModeControl < 180) |
173 | { |
173 | { |
174 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_AID; |
174 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_AID; |
175 | NCFlags &= ~(NC_FLAG_FREE | NC_FLAG_CH); |
175 | NCFlags &= ~(NC_FLAG_FREE | NC_FLAG_CH); |
176 | NCFlags |= NC_FLAG_PH; |
176 | NCFlags |= NC_FLAG_PH; |
177 | } |
177 | } |
178 | else |
178 | else |
179 | { |
179 | { |
180 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_WAYPOINT; |
180 | GPS_Parameter.FlightMode = GPS_FLIGHT_MODE_WAYPOINT; |
181 | NCFlags &= ~(NC_FLAG_FREE | NC_FLAG_PH); |
181 | NCFlags &= ~(NC_FLAG_FREE | NC_FLAG_PH); |
182 | NCFlags |= NC_FLAG_CH; |
182 | NCFlags |= NC_FLAG_CH; |
183 | } |
183 | } |
184 | } |
184 | } |
185 | GPS_Parameter.Gain = (float)Parameter.NaviGpsGain; |
185 | GPS_Parameter.Gain = (float)Parameter.NaviGpsGain; |
186 | GPS_Parameter.P = (float)Parameter.NaviGpsP; |
186 | GPS_Parameter.P = (float)Parameter.NaviGpsP; |
187 | GPS_Parameter.I = (float)Parameter.NaviGpsI; |
187 | GPS_Parameter.I = (float)Parameter.NaviGpsI; |
188 | GPS_Parameter.D = (float)Parameter.NaviGpsD; |
188 | GPS_Parameter.D = (float)Parameter.NaviGpsD; |
189 | GPS_Parameter.A = (float)Parameter.NaviGpsD; |
189 | GPS_Parameter.A = (float)Parameter.NaviGpsD; |
190 | GPS_Parameter.ACC = (float)Parameter.NaviGpsACC; |
190 | GPS_Parameter.ACC = (float)Parameter.NaviGpsACC; |
191 | GPS_Parameter.P_Limit = (u32)Parameter.NaviGpsPLimit; |
191 | GPS_Parameter.P_Limit = (s32)Parameter.NaviGpsPLimit; |
192 | GPS_Parameter.I_Limit = (u32)Parameter.NaviGpsILimit; |
192 | GPS_Parameter.I_Limit = (s32)Parameter.NaviGpsILimit; |
193 | GPS_Parameter.D_Limit = (u32)Parameter.NaviGpsDLimit; |
193 | GPS_Parameter.D_Limit = (s32)Parameter.NaviGpsDLimit; |
194 | GPS_Parameter.PID_Limit = 2* (u32)Parameter.NaviAngleLimitation; |
194 | GPS_Parameter.PID_Limit = 2* (u32)Parameter.NaviAngleLimitation; |
195 | GPS_Parameter.BrakingDuration = (u32)Parameter.NaviPH_LoginTime; |
195 | GPS_Parameter.BrakingDuration = (u32)Parameter.NaviPH_LoginTime; |
196 | GPS_Parameter.SpeedCompensation = (float)Parameter.NaviSpeedCompensation; |
196 | GPS_Parameter.SpeedCompensation = (float)Parameter.NaviSpeedCompensation; |
197 | GPS_Parameter.MinSat = (u8)Parameter.NaviGpsMinSat; |
197 | GPS_Parameter.MinSat = (u8)Parameter.NaviGpsMinSat; |
198 | GPS_Parameter.StickThreshold = (s8)Parameter.NaviStickThreshold; |
198 | GPS_Parameter.StickThreshold = (s8)Parameter.NaviStickThreshold; |
199 | GPS_Parameter.WindCorrection = (float)Parameter.NaviWindCorrection; |
199 | GPS_Parameter.WindCorrection = (float)Parameter.NaviWindCorrection; |
200 | GPS_Parameter.OperatingRadius = (u32)Parameter.NaviOperatingRadius * 100; // conversion of m to cm |
200 | GPS_Parameter.OperatingRadius = (s32)Parameter.NaviOperatingRadius * 100; // conversion of m to cm |
201 | } |
201 | } |
202 | // FlightMode changed? |
202 | // FlightMode changed? |
203 | if(GPS_Parameter.FlightMode != FlightMode_Old) BeepTime = 100; // beep to indicate that mode has switched |
203 | if(GPS_Parameter.FlightMode != FlightMode_Old) BeepTime = 100; // beep to indicate that mode has switched |
204 | FlightMode_Old = GPS_Parameter.FlightMode; |
204 | FlightMode_Old = GPS_Parameter.FlightMode; |
205 | } |
205 | } |
206 | 206 | ||
207 | //------------------------------------------------------------- |
207 | //------------------------------------------------------------- |
208 | // This function defines a good GPS signal condition |
208 | // This function defines a good GPS signal condition |
209 | u8 GPS_IsSignalOK(void) |
209 | u8 GPS_IsSignalOK(void) |
210 | { |
210 | { |
211 | if( (GPSData.Status != INVALID) && (GPSData.SatFix == SATFIX_3D) && (GPSData.NumOfSats >= GPS_Parameter.MinSat)) return(1); |
211 | if( (GPSData.Status != INVALID) && (GPSData.SatFix == SATFIX_3D) && (GPSData.NumOfSats >= GPS_Parameter.MinSat)) return(1); |
212 | else return(0); |
212 | else return(0); |
213 | } |
213 | } |
214 | 214 | ||
215 | //------------------------------------------------------------ |
215 | //------------------------------------------------------------ |
216 | // Checks for manual control action |
216 | // Checks for manual control action |
217 | u8 GPS_IsManuallyControlled(void) |
217 | u8 GPS_IsManuallyControlled(void) |
218 | { |
218 | { |
219 | if( ( (abs(FC.StickNick) > GPS_Parameter.StickThreshold) || (abs(FC.StickRoll) > GPS_Parameter.StickThreshold)) && (GPS_Parameter.StickThreshold > 0)) return 1; |
219 | if( ( (abs(FC.StickNick) > GPS_Parameter.StickThreshold) || (abs(FC.StickRoll) > GPS_Parameter.StickThreshold)) && (GPS_Parameter.StickThreshold > 0) && (FC.RC_Quality > 150) ) |
- | 220 | { |
|
- | 221 | NCFlags |= NC_FLAG_MANUAL_CONTROL; |
|
- | 222 | return(1); |
|
- | 223 | } |
|
- | 224 | else |
|
- | 225 | { |
|
- | 226 | NCFlags &= ~NC_FLAG_MANUAL_CONTROL; |
|
220 | else return 0; |
227 | return(0); |
- | 228 | } |
|
221 | } |
229 | } |
222 | 230 | ||
223 | //------------------------------------------------------------ |
231 | //------------------------------------------------------------ |
224 | // copy GPS position from source position to target position |
232 | // copy GPS position from source position to target position |
225 | u8 GPS_CopyPosition(GPS_Pos_t * pGPSPosSrc, GPS_Pos_t* pGPSPosTgt) |
233 | u8 GPS_CopyPosition(GPS_Pos_t * pGPSPosSrc, GPS_Pos_t* pGPSPosTgt) |
226 | { |
234 | { |
227 | u8 retval = 0; |
235 | u8 retval = 0; |
228 | if((pGPSPosSrc == NULL) || (pGPSPosTgt == NULL)) return(retval); // bad pointer |
236 | if((pGPSPosSrc == NULL) || (pGPSPosTgt == NULL)) return(retval); // bad pointer |
229 | // copy only valid positions |
237 | // copy only valid positions |
230 | if(pGPSPosSrc->Status != INVALID) |
238 | if(pGPSPosSrc->Status != INVALID) |
231 | { |
239 | { |
232 | // if the source GPS position is not invalid |
240 | // if the source GPS position is not invalid |
233 | pGPSPosTgt->Longitude = pGPSPosSrc->Longitude; |
241 | pGPSPosTgt->Longitude = pGPSPosSrc->Longitude; |
234 | pGPSPosTgt->Latitude = pGPSPosSrc->Latitude; |
242 | pGPSPosTgt->Latitude = pGPSPosSrc->Latitude; |
235 | pGPSPosTgt->Altitude = pGPSPosSrc->Altitude; |
243 | pGPSPosTgt->Altitude = pGPSPosSrc->Altitude; |
236 | pGPSPosTgt->Status = NEWDATA; // mark data in target position as new |
244 | pGPSPosTgt->Status = NEWDATA; // mark data in target position as new |
237 | retval = 1; |
245 | retval = 1; |
238 | } |
246 | } |
239 | return(retval); |
247 | return(retval); |
240 | } |
248 | } |
241 | 249 | ||
242 | //------------------------------------------------------------ |
250 | //------------------------------------------------------------ |
243 | // clear position data |
251 | // clear position data |
244 | u8 GPS_ClearPosition(GPS_Pos_t * pGPSPos) |
252 | u8 GPS_ClearPosition(GPS_Pos_t * pGPSPos) |
245 | { |
253 | { |
246 | u8 retval = FALSE; |
254 | u8 retval = FALSE; |
247 | if(pGPSPos == NULL) return(retval); // bad pointer |
255 | if(pGPSPos == NULL) return(retval); // bad pointer |
248 | else |
256 | else |
249 | { |
257 | { |
250 | pGPSPos->Longitude = 0; |
258 | pGPSPos->Longitude = 0; |
251 | pGPSPos->Latitude = 0; |
259 | pGPSPos->Latitude = 0; |
252 | pGPSPos->Altitude = 0; |
260 | pGPSPos->Altitude = 0; |
253 | pGPSPos->Status = INVALID; |
261 | pGPSPos->Status = INVALID; |
254 | retval = TRUE; |
262 | retval = TRUE; |
255 | } |
263 | } |
256 | return (retval); |
264 | return (retval); |
257 | } |
265 | } |
258 | 266 | ||
259 | 267 | ||
260 | //------------------------------------------------------------ |
268 | //------------------------------------------------------------ |
261 | void GPS_Neutral(void) |
269 | void GPS_Neutral(void) |
262 | { |
270 | { |
263 | GPS_Stick.Nick = 0; |
271 | GPS_Stick.Nick = 0; |
264 | GPS_Stick.Roll = 0; |
272 | GPS_Stick.Roll = 0; |
265 | GPS_Stick.Yaw = 0; |
273 | GPS_Stick.Yaw = 0; |
266 | } |
274 | } |
267 | 275 | ||
268 | //------------------------------------------------------------ |
276 | //------------------------------------------------------------ |
269 | void GPS_Init(void) |
277 | void GPS_Init(void) |
270 | { |
278 | { |
271 | SerialPutString("\r\n GPS init..."); |
279 | SerialPutString("\r\n GPS init..."); |
272 | UBX_Init(); |
280 | UBX_Init(); |
273 | GPS_Neutral(); |
281 | GPS_Neutral(); |
274 | GPS_ClearPosition(&GPS_HoldPosition); |
282 | GPS_ClearPosition(&GPS_HoldPosition); |
275 | GPS_ClearPosition(&GPS_HomePosition); |
283 | GPS_ClearPosition(&GPS_HomePosition); |
276 | GPS_pTargetPosition = NULL; |
284 | GPS_pTargetPosition = NULL; |
277 | WPList_Init(); |
285 | WPList_Init(); |
278 | GPS_pWaypoint = WPList_Begin(); |
286 | GPS_pWaypoint = WPList_Begin(); |
279 | GPS_UpdateParameter(); |
287 | GPS_UpdateParameter(); |
280 | SerialPutString("ok"); |
288 | SerialPutString("ok"); |
281 | } |
289 | } |
282 | 290 | ||
283 | //------------------------------------------------------------ |
291 | //------------------------------------------------------------ |
284 | // calculate the bearing to target position from its deviation |
292 | // calculate the bearing to target position from its deviation |
285 | s32 DirectionToTarget_N_E(float northdev, float eastdev) |
293 | s32 DirectionToTarget_N_E(float northdev, float eastdev) |
286 | { |
294 | { |
287 | s32 bearing; |
295 | s32 bearing; |
288 | bearing = (s32)(atan2(northdev, eastdev) / M_PI_180); |
296 | bearing = (s32)(atan2(northdev, eastdev) / M_PI_180); |
289 | bearing = (270L - bearing)%360L; |
297 | bearing = (270L - bearing)%360L; |
290 | return(bearing); |
298 | return(bearing); |
291 | } |
299 | } |
292 | 300 | ||
293 | 301 | ||
294 | //------------------------------------------------------------ |
302 | //------------------------------------------------------------ |
295 | // Rescale xy-vector length if length limit is violated |
303 | // Rescale xy-vector length if length limit is violated |
296 | // return vector length after scaling |
304 | // returns vector len after scaling |
297 | u32 GPS_LimitXY(s32 *x, s32 *y, u32 limit) |
305 | s32 GPS_LimitXY(s32 *x, s32 *y, s32 limit) |
298 | { |
306 | { |
299 | u32 dist; |
307 | s32 dist; |
300 | 308 | ||
301 | dist = (u32)hypot(*x,*y); // the length of the vector |
309 | dist = (s32)hypot(*x,*y); // the length of the vector |
302 | if (dist > limit) |
310 | if (dist > limit) |
303 | // if vector length is larger than the given limit |
311 | // if vector length is larger than the given limit |
304 | { // scale vector compontents so that the length is cut off to limit |
312 | { // scale vector compontents so that the length is cut off to limit |
305 | *x = (s32)(((double)(*x) * (double)limit) / dist); |
313 | *x = (s32)(( (double)(*x) * (double)limit ) / (double)dist); |
306 | *y = (s32)(((double)(*y) * (double)limit) / dist); |
314 | *y = (s32)(( (double)(*y) * (double)limit ) / (double)dist); |
307 | dist = limit; |
315 | dist = limit; |
308 | } |
316 | } |
309 | return(dist); |
317 | return(dist); |
310 | } |
318 | } |
311 | 319 | ||
312 | //------------------------------------------------------------ |
320 | //------------------------------------------------------------ |
313 | // transform the integer deg into float radians |
321 | // transform the integer deg into float radians |
314 | inline double RadiansFromGPS(s32 deg) |
322 | inline double RadiansFromGPS(s32 deg) |
315 | { |
323 | { |
316 | return ((double)deg * 1e-7f * M_PI_180); // 1E-7 because deg is the value in ° * 1E7 |
324 | return ((double)deg * 1e-7f * M_PI_180); // 1E-7 because deg is the value in ° * 1E7 |
317 | } |
325 | } |
318 | 326 | ||
319 | //------------------------------------------------------------ |
327 | //------------------------------------------------------------ |
320 | // transform the integer deg into float deg |
328 | // transform the integer deg into float deg |
321 | inline double DegFromGPS(s32 deg) |
329 | inline double DegFromGPS(s32 deg) |
322 | { |
330 | { |
323 | return ((double)deg * 1e-7f); // 1E-7 because deg is the value in ° * 1E7 |
331 | return ((double)deg * 1e-7f); // 1E-7 because deg is the value in ° * 1E7 |
324 | } |
332 | } |
325 | 333 | ||
326 | //------------------------------------------------------------ |
334 | //------------------------------------------------------------ |
327 | // calculate the deviation from the current position to the target position |
335 | // calculate the deviation from the current position to the target position |
328 | u8 GPS_CalculateDeviation(GPS_Pos_t * pCurrentPos, GPS_Pos_t * pTargetPos, GPS_Deviation_t* pDeviationFromTarget) |
336 | u8 GPS_CalculateDeviation(GPS_Pos_t * pCurrentPos, GPS_Pos_t * pTargetPos, GPS_Deviation_t* pDeviationFromTarget) |
329 | { |
337 | { |
330 | double temp1, temp2; |
338 | double temp1, temp2; |
331 | // if given pointer is NULL |
339 | // if given pointer is NULL |
332 | if((pCurrentPos == NULL) || (pTargetPos == NULL)) goto baddata; |
340 | if((pCurrentPos == NULL) || (pTargetPos == NULL)) goto baddata; |
333 | // if positions are invalid |
341 | // if positions are invalid |
334 | if((pCurrentPos->Status == INVALID) || (pTargetPos->Status == INVALID)) goto baddata; |
342 | if((pCurrentPos->Status == INVALID) || (pTargetPos->Status == INVALID)) goto baddata; |
335 | 343 | ||
336 | // The deviation from the current to the target position along north and east direction is |
344 | // The deviation from the current to the target position along north and east direction is |
337 | // simple the lat/lon difference. To convert that angular deviation into an |
345 | // simple the lat/lon difference. To convert that angular deviation into an |
338 | // arc length the spherical projection has to be considered. |
346 | // arc length the spherical projection has to be considered. |
339 | // The mean earth radius is 6371km. Therfore the arc length per latitude degree |
347 | // The mean earth radius is 6371km. Therfore the arc length per latitude degree |
340 | // is always 6371km * 2 * Pi / 360deg = 111.2 km/deg. |
348 | // is always 6371km * 2 * Pi / 360deg = 111.2 km/deg. |
341 | // The arc length per longitude degree depends on the correspondig latitude and |
349 | // The arc length per longitude degree depends on the correspondig latitude and |
342 | // is 111.2km * cos(latitude). |
350 | // is 111.2km * cos(latitude). |
343 | 351 | ||
344 | // calculate the shortest longitude deviation from target |
352 | // calculate the shortest longitude deviation from target |
345 | temp1 = DegFromGPS(pCurrentPos->Longitude) - DegFromGPS(pTargetPos->Longitude); |
353 | temp1 = DegFromGPS(pCurrentPos->Longitude) - DegFromGPS(pTargetPos->Longitude); |
346 | // outside an angular difference of -180 deg ... +180 deg its shorter to go the other way around |
354 | // outside an angular difference of -180 deg ... +180 deg its shorter to go the other way around |
347 | // In our application we wont fly more than 20.000 km but along the date line this is important. |
355 | // In our application we wont fly more than 20.000 km but along the date line this is important. |
348 | if(temp1 > 180.0f) temp1 -= 360.0f; |
356 | if(temp1 > 180.0f) temp1 -= 360.0f; |
349 | else if (temp1 < -180.0f) temp1 += 360.0f; |
357 | else if (temp1 < -180.0f) temp1 += 360.0f; |
350 | temp1 *= cos((RadiansFromGPS(pTargetPos->Latitude) + RadiansFromGPS(pCurrentPos->Latitude))/2); |
358 | temp1 *= cos((RadiansFromGPS(pTargetPos->Latitude) + RadiansFromGPS(pCurrentPos->Latitude))/2); |
351 | // calculate latitude deviation from target |
359 | // calculate latitude deviation from target |
352 | // this is allways within -180 deg ... 180 deg |
360 | // this is allways within -180 deg ... 180 deg |
353 | temp2 = DegFromGPS(pCurrentPos->Latitude) - DegFromGPS(pTargetPos->Latitude); |
361 | temp2 = DegFromGPS(pCurrentPos->Latitude) - DegFromGPS(pTargetPos->Latitude); |
354 | // deviation from target position in cm |
362 | // deviation from target position in cm |
355 | // i.e. the distance to walk from the target in northern and eastern direction to reach the current position |
363 | // i.e. the distance to walk from the target in northern and eastern direction to reach the current position |
356 | 364 | ||
357 | pDeviationFromTarget->Status = INVALID; |
365 | pDeviationFromTarget->Status = INVALID; |
358 | pDeviationFromTarget->North = (s32)(11119492.7f * temp2); |
366 | pDeviationFromTarget->North = (s32)(11119492.7f * temp2); |
359 | pDeviationFromTarget->East = (s32)(11119492.7f * temp1); |
367 | pDeviationFromTarget->East = (s32)(11119492.7f * temp1); |
360 | // If the position deviation is small enough to neglect the earth curvature |
368 | // If the position deviation is small enough to neglect the earth curvature |
361 | // (this is for our application always fulfilled) the distance to target |
369 | // (this is for our application always fulfilled) the distance to target |
362 | // can be calculated by the pythagoras of north and east deviation. |
370 | // can be calculated by the pythagoras of north and east deviation. |
363 | pDeviationFromTarget->Distance = (u32)(11119492.7f * hypot(temp1, temp2)); |
371 | pDeviationFromTarget->Distance = (s32)(11119492.7f * hypot(temp1, temp2)); |
364 | if (pDeviationFromTarget->Distance == 0L) pDeviationFromTarget->Bearing = 0L; |
372 | if (pDeviationFromTarget->Distance == 0L) pDeviationFromTarget->Bearing = 0L; |
365 | else pDeviationFromTarget->Bearing = DirectionToTarget_N_E(temp2, temp1); |
373 | else pDeviationFromTarget->Bearing = DirectionToTarget_N_E(temp2, temp1); |
366 | pDeviationFromTarget->Status = NEWDATA; |
374 | pDeviationFromTarget->Status = NEWDATA; |
367 | return TRUE; |
375 | return TRUE; |
368 | 376 | ||
369 | baddata: |
377 | baddata: |
370 | pDeviationFromTarget->North = 0L; |
378 | pDeviationFromTarget->North = 0L; |
371 | pDeviationFromTarget->East = 0L; |
379 | pDeviationFromTarget->East = 0L; |
372 | pDeviationFromTarget->Distance = 0L; |
380 | pDeviationFromTarget->Distance = 0L; |
373 | pDeviationFromTarget->Bearing = 0L; |
381 | pDeviationFromTarget->Bearing = 0L; |
374 | pDeviationFromTarget->Status = INVALID; |
382 | pDeviationFromTarget->Status = INVALID; |
375 | return FALSE; |
383 | return FALSE; |
376 | } |
384 | } |
377 | 385 | ||
378 | //------------------------------------------------------------ |
386 | //------------------------------------------------------------ |
379 | void GPS_Navigation(void) |
387 | void GPS_Navigation(void) |
380 | { |
388 | { |
381 | static u32 beep_rythm; |
389 | static u32 beep_rythm; |
382 | static u32 GPSDataTimeout = 0; |
390 | static u32 GPSDataTimeout = 0; |
383 | 391 | ||
384 | // pointer to current target position |
392 | // pointer to current target position |
385 | static GPS_Pos_t * pTargetPositionOld = NULL; |
393 | static GPS_Pos_t * pTargetPositionOld = NULL; |
386 | static Waypoint_t* GPS_pWaypointOld = NULL; |
394 | static Waypoint_t* GPS_pWaypointOld = NULL; |
387 | 395 | ||
388 | static GPS_Pos_t RangedTargetPosition = {0,0,0, INVALID}; // the limited target position, this is derived from the target position with repect to the operating radius |
396 | static GPS_Pos_t RangedTargetPosition = {0,0,0, INVALID}; // the limited target position, this is derived from the target position with repect to the operating radius |
389 | static u32 OperatingRadiusOld = -1; |
397 | static s32 OperatingRadiusOld = -1; |
390 | static u32 WPTime = 0; |
398 | static u32 WPTime = 0; |
391 | 399 | ||
392 | //++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
400 | //++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
393 | //+ Check for new data from GPS-receiver |
401 | //+ Check for new data from GPS-receiver |
394 | //++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
402 | //++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
395 | switch(GPSData.Status) |
403 | switch(GPSData.Status) |
396 | { |
404 | { |
397 | case INVALID: // no gps data available |
405 | case INVALID: // no gps data available |
398 | // do nothing |
406 | // do nothing |
399 | GPS_Parameter.PID_Limit = 0; // disables PID output |
407 | GPS_Parameter.PID_Limit = 0; // disables PID output |
400 | break; |
408 | break; |
401 | 409 | ||
402 | case PROCESSED: // the current data have been allready processed |
410 | case PROCESSED: // the current data have been allready processed |
403 | // if no new data are available within the timeout switch to invalid state. |
411 | // if no new data are available within the timeout switch to invalid state. |
404 | if(CheckDelay(GPSDataTimeout)) GPSData.Status = INVALID; |
412 | if(CheckDelay(GPSDataTimeout)) GPSData.Status = INVALID; |
405 | // wait for new gps data |
413 | // wait for new gps data |
406 | break; |
414 | break; |
407 | 415 | ||
408 | case NEWDATA: // handle new gps data |
416 | case NEWDATA: // handle new gps data |
409 | 417 | ||
410 | // update GPS Parameter from FC-Data via SPI interface |
418 | // update GPS Parameter from FC-Data via SPI interface |
411 | GPS_UpdateParameter(); |
419 | GPS_UpdateParameter(); |
412 | 420 | ||
413 | // wait maximum of 3 times the normal data update time before data timemout |
421 | // wait maximum of 3 times the normal data update time before data timemout |
414 | GPSDataTimeout = SetDelay(3 * GPS_UPDATETIME_MS); |
422 | GPSDataTimeout = SetDelay(3 * GPS_UPDATETIME_MS); |
415 | beep_rythm++; |
423 | beep_rythm++; |
416 | 424 | ||
417 | // debug |
425 | // debug |
418 | DebugOut.Analog[21] = (s16)GPSData.Speed_North; |
426 | DebugOut.Analog[21] = (s16)GPSData.Speed_North; |
419 | DebugOut.Analog[22] = (s16)GPSData.Speed_East; |
427 | DebugOut.Analog[22] = (s16)GPSData.Speed_East; |
420 | DebugOut.Analog[31] = (s16)GPSData.NumOfSats; |
428 | DebugOut.Analog[31] = (s16)GPSData.NumOfSats; |
421 | 429 | ||
422 | // If GPS signal condition is sufficient for a reliable position measurement |
430 | // If GPS signal condition is sufficient for a reliable position measurement |
423 | if(GPS_IsSignalOK()) |
431 | if(GPS_IsSignalOK()) |
424 | { |
432 | { |
425 | // update home deviation info |
433 | // update home deviation info |
426 | GPS_CalculateDeviation(&(GPSData.Position), &GPS_HomePosition, &CurrentHomeDeviation); |
434 | GPS_CalculateDeviation(&(GPSData.Position), &GPS_HomePosition, &CurrentHomeDeviation); |
427 | 435 | ||
428 | // if the MK is starting or the home position is invalid then store the home position |
436 | // if the MK is starting or the home position is invalid then store the home position |
429 | if((FC.MKFlags & MKFLAG_START) || (GPS_HomePosition.Status == INVALID)) |
437 | if((FC.MKFlags & MKFLAG_START) || (GPS_HomePosition.Status == INVALID)) |
430 | { // try to update the home position from the current position |
438 | { // try to update the home position from the current position |
431 | if(GPS_CopyPosition(&(GPSData.Position), &GPS_HomePosition)) |
439 | if(GPS_CopyPosition(&(GPSData.Position), &GPS_HomePosition)) |
432 | { |
440 | { |
433 | BeepTime = 700; // beep on success |
441 | BeepTime = 700; // beep on success |
434 | GPS_CopyPosition(&GPS_HomePosition, &(NaviData.HomePosition)); |
442 | GPS_CopyPosition(&GPS_HomePosition, &(NaviData.HomePosition)); |
435 | } |
443 | } |
436 | GPS_pWaypoint = WPList_Begin(); // go to start of waypoint list, return NULL of the list is empty |
444 | GPS_pWaypoint = WPList_Begin(); // go to start of waypoint list, return NULL of the list is empty |
437 | } |
445 | } |
438 | 446 | ||
439 | /* The selected flight mode influences the target position pointer and therefore the behavior */ |
447 | /* The selected flight mode influences the target position pointer and therefore the behavior */ |
440 | 448 | ||
441 | // check for current flight mode and set the target pointer GPS_pTargetPosition respectively |
449 | // check for current flight mode and set the target pointer GPS_pTargetPosition respectively |
442 | switch(GPS_Parameter.FlightMode) |
450 | switch(GPS_Parameter.FlightMode) |
443 | { |
451 | { |
444 | // the GPS control is deactived |
452 | // the GPS control is deactived |
445 | case GPS_FLIGHT_MODE_FREE: |
453 | case GPS_FLIGHT_MODE_FREE: |
446 | 454 | ||
447 | GPS_Parameter.PID_Limit = 0; // disables PID output |
455 | GPS_Parameter.PID_Limit = 0; // disables PID output |
448 | // update hold position |
456 | // update hold position |
449 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
457 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
450 | // no target position |
458 | // no target position |
451 | GPS_pTargetPosition = NULL; |
459 | GPS_pTargetPosition = NULL; |
452 | GPS_TargetRadius = 0; |
460 | GPS_TargetRadius = 0; |
453 | break; |
461 | break; |
454 | 462 | ||
455 | // the GPS supports the position hold, if the pilot takes no action |
463 | // the GPS supports the position hold, if the pilot takes no action |
456 | case GPS_FLIGHT_MODE_AID: |
464 | case GPS_FLIGHT_MODE_AID: |
457 | 465 | ||
458 | // reset WPList to begin |
466 | // reset WPList to begin |
459 | GPS_pWaypoint = WPList_Begin(); |
467 | GPS_pWaypoint = WPList_Begin(); |
460 | 468 | ||
461 | if(GPS_IsManuallyControlled()) |
469 | if(GPS_IsManuallyControlled()) |
462 | { |
470 | { |
463 | GPS_Parameter.PID_Limit = 0; // disables PID output, as long as the manual conrol is active |
471 | GPS_Parameter.PID_Limit = 0; // disables PID output, as long as the manual conrol is active |
464 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
472 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
465 | GPS_pTargetPosition = NULL; |
473 | GPS_pTargetPosition = NULL; |
466 | GPS_TargetRadius = 0; |
474 | GPS_TargetRadius = 0; |
467 | } |
475 | } |
468 | else |
476 | else |
469 | { |
477 | { |
470 | GPS_pTargetPosition = &GPS_HoldPosition; |
478 | GPS_pTargetPosition = &GPS_HoldPosition; |
471 | GPS_TargetRadius = 100; // 1 meter |
479 | GPS_TargetRadius = 100; // 1 meter |
472 | } |
480 | } |
473 | break; |
481 | break; |
474 | 482 | ||
475 | // the GPS control is directed to a target position |
483 | // the GPS control is directed to a target position |
476 | // given by a waypoint or by the home position |
484 | // given by a waypoint or by the home position |
477 | case GPS_FLIGHT_MODE_WAYPOINT: |
485 | case GPS_FLIGHT_MODE_WAYPOINT: |
478 | 486 | ||
479 | if(GPS_IsManuallyControlled()) // the human pilot takes the action |
487 | if(GPS_IsManuallyControlled()) // the human pilot takes the action |
480 | { |
488 | { |
481 | GPS_Parameter.PID_Limit = 0; // disables PID output, as long as the manual conrol is active |
489 | GPS_Parameter.PID_Limit = 0; // disables PID output, as long as the manual conrol is active |
482 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); // update hold position |
490 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); // update hold position |
483 | GPS_pTargetPosition = NULL; // set target position invalid |
491 | GPS_pTargetPosition = NULL; // set target position invalid |
484 | GPS_TargetRadius = 0; |
492 | GPS_TargetRadius = 0; |
485 | } |
493 | } |
486 | else // no manual control -> gps position hold active |
494 | else // no manual control -> gps position hold active |
487 | { |
495 | { |
488 | // waypoint trigger logic |
496 | // waypoint trigger logic |
489 | if(GPS_pWaypoint != NULL) // waypoint exist |
497 | if(GPS_pWaypoint != NULL) // waypoint exist |
490 | { |
498 | { |
491 | if(GPS_pWaypoint->Position.Status == INVALID) // should never happen |
499 | if(GPS_pWaypoint->Position.Status == INVALID) // should never happen |
492 | { |
500 | { |
493 | GPS_pWaypoint = WPList_Next(); // goto to next WP |
501 | GPS_pWaypoint = WPList_Next(); // goto to next WP |
494 | BeepTime = 255; |
502 | BeepTime = 255; |
495 | } |
503 | } |
496 | else // waypoint position is valid |
504 | else // waypoint position is valid |
497 | { |
505 | { |
498 | // check if the pointer to the waypoint has been changed or the data have been updated |
506 | // check if the pointer to the waypoint has been changed or the data have been updated |
499 | if((GPS_pWaypoint != GPS_pWaypointOld) || (GPS_pWaypoint->Position.Status == NEWDATA)) |
507 | if((GPS_pWaypoint != GPS_pWaypointOld) || (GPS_pWaypoint->Position.Status == NEWDATA)) |
500 | { |
508 | { |
501 | GPS_pWaypointOld = GPS_pWaypoint; |
509 | GPS_pWaypointOld = GPS_pWaypoint; |
502 | } |
510 | } |
503 | // if WP has been reached once, wait hold time before trigger to next one |
511 | // if WP has been reached once, wait hold time before trigger to next one |
504 | if(NCFlags & NC_FLAG_TARGET_REACHED) |
512 | if(NCFlags & NC_FLAG_TARGET_REACHED) |
505 | { |
513 | { |
506 | /* ToDo: Adjust GPS_pWaypoint->Heading, GPS_pWaypoint->Event handling */ |
514 | /* ToDo: Adjust GPS_pWaypoint->Heading, GPS_pWaypoint->Event handling */ |
507 | if(CheckDelay(WPTime)) |
515 | if(CheckDelay(WPTime)) |
508 | { |
516 | { |
509 | GPS_pWaypoint = WPList_Next(); // goto to next waypoint, return NULL if end of list has been reached |
517 | GPS_pWaypoint = WPList_Next(); // goto to next waypoint, return NULL if end of list has been reached |
510 | } |
518 | } |
511 | } // EOF if(WPArrived) |
519 | } // EOF if(WPArrived) |
512 | else |
520 | else |
513 | { |
521 | { |
514 | WPTime = SetDelay(GPS_pWaypoint->HoldTime * 1000); // set hold time stamp |
522 | WPTime = SetDelay(GPS_pWaypoint->HoldTime * 1000); // set hold time stamp |
515 | } |
523 | } |
516 | } |
524 | } |
517 | } // EOF waypoint trigger logic |
525 | } // EOF waypoint trigger logic |
518 | 526 | ||
519 | if(GPS_pWaypoint != NULL) // Waypoint exist |
527 | if(GPS_pWaypoint != NULL) // Waypoint exist |
520 | { |
528 | { |
521 | // update the hold position |
529 | // update the hold position |
522 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
530 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
523 | GPS_pTargetPosition = &(GPS_pWaypoint->Position); |
531 | GPS_pTargetPosition = &(GPS_pWaypoint->Position); |
524 | GPS_TargetRadius = (u32)(GPS_pWaypoint->ToleranceRadius) * 100L; |
532 | GPS_TargetRadius = (s32)(GPS_pWaypoint->ToleranceRadius) * 100L; |
525 | 533 | ||
526 | } |
534 | } |
527 | else // no waypoint info available, i.e. the WPList is empty or the end of the list has been reached |
535 | else // no waypoint info available, i.e. the WPList is empty or the end of the list has been reached |
528 | { |
536 | { |
529 | // fly back to home postion |
537 | // fly back to home postion |
530 | if(GPS_HomePosition.Status == INVALID) |
538 | if(GPS_HomePosition.Status == INVALID) |
531 | { |
539 | { |
532 | GPS_pTargetPosition = &GPS_HoldPosition; // fall back to hold mode if home position is not available |
540 | GPS_pTargetPosition = &GPS_HoldPosition; // fall back to hold mode if home position is not available |
533 | GPS_TargetRadius = 100; |
541 | GPS_TargetRadius = 100; |
534 | BeepTime = 255; // beep to indicate missin home position |
542 | BeepTime = 255; // beep to indicate missin home position |
535 | } |
543 | } |
536 | else // the home position is valid |
544 | else // the home position is valid |
537 | { |
545 | { |
538 | // update the hold position |
546 | // update the hold position |
539 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
547 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
540 | // set target to home position |
548 | // set target to home position |
541 | GPS_pTargetPosition = &GPS_HomePosition; |
549 | GPS_pTargetPosition = &GPS_HomePosition; |
542 | GPS_TargetRadius = 100; |
550 | GPS_TargetRadius = 100; |
543 | } |
551 | } |
544 | } |
552 | } |
545 | } // EOF no manual control |
553 | } // EOF no manual control |
546 | break; |
554 | break; |
547 | 555 | ||
548 | case GPS_FLIGHT_MODE_UNDEF: |
556 | case GPS_FLIGHT_MODE_UNDEF: |
549 | default: |
557 | default: |
550 | GPS_Parameter.PID_Limit = 0; // disables PID output |
558 | GPS_Parameter.PID_Limit = 0; // disables PID output |
551 | // update hold position |
559 | // update hold position |
552 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
560 | GPS_CopyPosition(&(GPSData.Position), &GPS_HoldPosition); |
553 | // no target position |
561 | // no target position |
554 | GPS_pTargetPosition = NULL; |
562 | GPS_pTargetPosition = NULL; |
555 | GPS_TargetRadius = 0; |
563 | GPS_TargetRadius = 0; |
556 | break; |
564 | break; |
557 | 565 | ||
558 | }// EOF GPS Mode Handling |
566 | }// EOF GPS Mode Handling |
559 | 567 | ||
560 | 568 | ||
561 | /* Calculation of range target based on the real target */ |
569 | /* Calculation of range target based on the real target */ |
562 | 570 | ||
563 | // if no target position exist clear the ranged target position |
571 | // if no target position exist clear the ranged target position |
564 | if(GPS_pTargetPosition == NULL) GPS_ClearPosition(&RangedTargetPosition); |
572 | if(GPS_pTargetPosition == NULL) GPS_ClearPosition(&RangedTargetPosition); |
565 | else |
573 | else |
566 | { // if the target position has been changed or the value has been updated or the OperatingRadius has changed |
574 | { // if the target position has been changed or the value has been updated or the OperatingRadius has changed |
567 | if((GPS_pTargetPosition != pTargetPositionOld) || (GPS_pTargetPosition->Status == NEWDATA) || (GPS_Parameter.OperatingRadius != OperatingRadiusOld) ) |
575 | if((GPS_pTargetPosition != pTargetPositionOld) || (GPS_pTargetPosition->Status == NEWDATA) || (GPS_Parameter.OperatingRadius != OperatingRadiusOld) ) |
568 | { |
576 | { |
569 | BeepTime = 255; // beep to indicate setting of a new target position |
577 | BeepTime = 255; // beep to indicate setting of a new target position |
570 | NCFlags &= ~NC_FLAG_TARGET_REACHED; // clear target reached flag |
578 | NCFlags &= ~NC_FLAG_TARGET_REACHED; // clear target reached flag |
571 | // calculate deviation of new target position from home position |
579 | // calculate deviation of new target position from home position |
572 | if(GPS_CalculateDeviation(GPS_pTargetPosition, &GPS_HomePosition, &TargetHomeDeviation)) |
580 | if(GPS_CalculateDeviation(GPS_pTargetPosition, &GPS_HomePosition, &TargetHomeDeviation)) |
573 | { |
581 | { |
574 | // check distance from home position |
582 | // check distance from home position |
575 | if(TargetHomeDeviation.Distance > GPS_Parameter.OperatingRadius) |
583 | if(TargetHomeDeviation.Distance > GPS_Parameter.OperatingRadius) |
576 | { |
584 | { |
577 | //calculate ranged target position to be within the operation radius area |
585 | //calculate ranged target position to be within the operation radius area |
578 | NCFlags |= NC_FLAG_RANGE_LIMIT; |
586 | NCFlags |= NC_FLAG_RANGE_LIMIT; |
579 | - | ||
580 | TargetHomeDeviation.North *= GPS_Parameter.OperatingRadius; |
587 | |
581 | TargetHomeDeviation.North /= TargetHomeDeviation.Distance; |
- | |
582 | TargetHomeDeviation.East *= GPS_Parameter.OperatingRadius; |
588 | TargetHomeDeviation.North = (s32)(((float)TargetHomeDeviation.North * (float)GPS_Parameter.OperatingRadius) / (float)TargetHomeDeviation.Distance); |
583 | TargetHomeDeviation.East /= TargetHomeDeviation.Distance; |
589 | TargetHomeDeviation.East = (s32)(((float)TargetHomeDeviation.East * (float)GPS_Parameter.OperatingRadius) / (float)TargetHomeDeviation.Distance); |
584 | TargetHomeDeviation.Distance = GPS_Parameter.OperatingRadius; |
590 | TargetHomeDeviation.Distance = GPS_Parameter.OperatingRadius; |
585 | 591 | ||
586 | RangedTargetPosition.Status = INVALID; |
592 | RangedTargetPosition.Status = INVALID; |
587 | RangedTargetPosition.Latitude = GPS_HomePosition.Latitude; |
593 | RangedTargetPosition.Latitude = GPS_HomePosition.Latitude; |
588 | RangedTargetPosition.Latitude += (s32)((float)TargetHomeDeviation.North / 1.11194927f); |
594 | RangedTargetPosition.Latitude += (s32)((float)TargetHomeDeviation.North / 1.11194927f); |
589 | RangedTargetPosition.Longitude = GPS_HomePosition.Longitude; |
595 | RangedTargetPosition.Longitude = GPS_HomePosition.Longitude; |
590 | RangedTargetPosition.Longitude += (s32)((float)TargetHomeDeviation.East / (1.11194927f * cos(RadiansFromGPS(GPS_HomePosition.Latitude))) ); |
596 | RangedTargetPosition.Longitude += (s32)((float)TargetHomeDeviation.East / (1.11194927f * cos(RadiansFromGPS(GPS_HomePosition.Latitude))) ); |
591 | RangedTargetPosition.Altitude = GPS_pTargetPosition->Altitude; |
597 | RangedTargetPosition.Altitude = GPS_pTargetPosition->Altitude; |
592 | RangedTargetPosition.Status = NEWDATA; |
598 | RangedTargetPosition.Status = NEWDATA; |
593 | } |
599 | } |
594 | else |
600 | else |
595 | { // the target is located within the operation radius area |
601 | { // the target is located within the operation radius area |
596 | // simple copy the loaction to the ranged target position |
602 | // simple copy the loaction to the ranged target position |
597 | GPS_CopyPosition(GPS_pTargetPosition, &RangedTargetPosition); |
603 | GPS_CopyPosition(GPS_pTargetPosition, &RangedTargetPosition); |
598 | NCFlags &= ~NC_FLAG_RANGE_LIMIT; |
604 | NCFlags &= ~NC_FLAG_RANGE_LIMIT; |
599 | } |
605 | } |
600 | } |
606 | } |
601 | else |
607 | else |
602 | { // deviation could not be determined |
608 | { // deviation could not be determined |
603 | GPS_ClearPosition(&RangedTargetPosition); |
609 | GPS_ClearPosition(&RangedTargetPosition); |
604 | } |
610 | } |
605 | GPS_pTargetPosition->Status = PROCESSED; // mark current target as processed! |
611 | GPS_pTargetPosition->Status = PROCESSED; // mark current target as processed! |
606 | } |
612 | } |
607 | } |
613 | } |
608 | OperatingRadiusOld = GPS_Parameter.OperatingRadius; |
614 | OperatingRadiusOld = GPS_Parameter.OperatingRadius; |
609 | // remember last target position pointer |
615 | // remember last target position pointer |
610 | pTargetPositionOld = GPS_pTargetPosition; |
616 | pTargetPositionOld = GPS_pTargetPosition; |
611 | 617 | ||
612 | /* Calculate position deviation from ranged target */ |
618 | /* Calculate position deviation from ranged target */ |
613 | 619 | ||
614 | // calculate deviation of current position to ranged target position in cm |
620 | // calculate deviation of current position to ranged target position in cm |
615 | if(GPS_CalculateDeviation(&(GPSData.Position), &RangedTargetPosition, &CurrentTargetDeviation)) |
621 | if(GPS_CalculateDeviation(&(GPSData.Position), &RangedTargetPosition, &CurrentTargetDeviation)) |
616 | { // set target reached flag of we once reached the target point |
622 | { // set target reached flag of we once reached the target point |
617 | if(!(NCFlags & NC_FLAG_TARGET_REACHED) && (CurrentTargetDeviation.Distance < GPS_TargetRadius)) |
623 | if(!(NCFlags & NC_FLAG_TARGET_REACHED) && (CurrentTargetDeviation.Distance < GPS_TargetRadius)) |
618 | { |
624 | { |
619 | NCFlags |= NC_FLAG_TARGET_REACHED; // set target reached flag |
625 | NCFlags |= NC_FLAG_TARGET_REACHED; // set target reached flag |
620 | } |
626 | } |
621 | // implement your control code here based |
627 | // implement your control code here based |
622 | // in the info available in the CurrentTargetDeviation, GPSData and FromFlightCtrl.GyroHeading |
628 | // in the info available in the CurrentTargetDeviation, GPSData and FromFlightCtrl.GyroHeading |
623 | GPS_Stick.Nick = 0; |
629 | GPS_Stick.Nick = 0; |
624 | GPS_Stick.Roll = 0; |
630 | GPS_Stick.Roll = 0; |
625 | GPS_Stick.Yaw = 0; |
631 | GPS_Stick.Yaw = 0; |
626 | } |
632 | } |
627 | else // deviation could not be calculated |
633 | else // deviation could not be calculated |
628 | { // do nothing on gps sticks! |
634 | { // do nothing on gps sticks! |
629 | GPS_Neutral(); |
635 | GPS_Neutral(); |
630 | } |
636 | } |
631 | 637 | ||
632 | }// eof if GPSSignal is OK |
638 | }// eof if GPSSignal is OK |
633 | else // GPSSignal not OK |
639 | else // GPSSignal not OK |
634 | { |
640 | { |
635 | GPS_Neutral(); |
641 | GPS_Neutral(); |
636 | // beep if signal is not sufficient |
642 | // beep if signal is not sufficient |
637 | if(GPS_Parameter.FlightMode != GPS_FLIGHT_MODE_FREE) |
643 | if(GPS_Parameter.FlightMode != GPS_FLIGHT_MODE_FREE) |
638 | { |
644 | { |
639 | if(!(GPSData.Flags & FLAG_GPSFIXOK) && !(beep_rythm % 5)) BeepTime = 100; |
645 | if(!(GPSData.Flags & FLAG_GPSFIXOK) && !(beep_rythm % 5)) BeepTime = 100; |
640 | else if (GPSData.NumOfSats < GPS_Parameter.MinSat && !(beep_rythm % 5)) BeepTime = 10; |
646 | else if (GPSData.NumOfSats < GPS_Parameter.MinSat && !(beep_rythm % 5)) BeepTime = 10; |
641 | } |
647 | } |
642 | } |
648 | } |
643 | GPSData.Status = PROCESSED; // mark as processed |
649 | GPSData.Status = PROCESSED; // mark as processed |
644 | break; |
650 | break; |
645 | } |
651 | } |
646 | 652 | ||
647 | DebugOut.Analog[6] = NCFlags; |
653 | DebugOut.Analog[6] = NCFlags; |
648 | DebugOut.Analog[27] = (s16)CurrentTargetDeviation.North; |
654 | DebugOut.Analog[27] = (s16)CurrentTargetDeviation.North; |
649 | DebugOut.Analog[28] = (s16)CurrentTargetDeviation.East; |
655 | DebugOut.Analog[28] = (s16)CurrentTargetDeviation.East; |
650 | DebugOut.Analog[29] = GPS_Stick.Nick; |
656 | DebugOut.Analog[29] = GPS_Stick.Nick; |
651 | DebugOut.Analog[30] = GPS_Stick.Roll; |
657 | DebugOut.Analog[30] = GPS_Stick.Roll; |
652 | 658 | ||
653 | // update navi data, send back to ground station |
659 | // update navi data, send back to ground station |
654 | GPS_CopyPosition(&(GPSData.Position), &(NaviData.CurrentPosition)); |
660 | GPS_CopyPosition(&(GPSData.Position), &(NaviData.CurrentPosition)); |
655 | GPS_CopyPosition(&RangedTargetPosition, &(NaviData.TargetPosition)); |
661 | GPS_CopyPosition(&RangedTargetPosition, &(NaviData.TargetPosition)); |
656 | GPS_CopyPosition(&GPS_HomePosition, &(NaviData.HomePosition)); |
662 | GPS_CopyPosition(&GPS_HomePosition, &(NaviData.HomePosition)); |
657 | NaviData.SatsInUse = GPSData.NumOfSats; |
663 | NaviData.SatsInUse = GPSData.NumOfSats; |
658 | NaviData.TargetPositionDeviation.Distance = (u16)CurrentTargetDeviation.Distance/10; // dm |
664 | NaviData.TargetPositionDeviation.Distance = (u16)CurrentTargetDeviation.Distance/10; // dm |
659 | NaviData.TargetPositionDeviation.Bearing = (s16)CurrentTargetDeviation.Bearing; |
665 | NaviData.TargetPositionDeviation.Bearing = (s16)CurrentTargetDeviation.Bearing; |
660 | NaviData.HomePositionDeviation.Distance = (u16)CurrentHomeDeviation.Distance/10; // dm |
666 | NaviData.HomePositionDeviation.Distance = (u16)CurrentHomeDeviation.Distance/10; // dm |
661 | NaviData.HomePositionDeviation.Bearing = (s16)CurrentHomeDeviation.Bearing; |
667 | NaviData.HomePositionDeviation.Bearing = (s16)CurrentHomeDeviation.Bearing; |
662 | NaviData.UBat = FC.UBat; |
668 | NaviData.UBat = FC.UBat; |
663 | NaviData.GroundSpeed = (u16)GPSData.Speed_Ground; |
669 | NaviData.GroundSpeed = (u16)GPSData.Speed_Ground; |
664 | NaviData.Heading = (s16)(GPSData.Heading/100000L); |
670 | NaviData.Heading = (s16)(GPSData.Heading/100000L); |
665 | NaviData.CompassHeading = (s16)FromFlightCtrl.GyroHeading/10; // in deg |
671 | NaviData.CompassHeading = (s16)FromFlightCtrl.GyroHeading/10; // in deg |
666 | NaviData.AngleNick = FromFlightCtrl.AngleNick / 10; // in deg |
672 | NaviData.AngleNick = FromFlightCtrl.AngleNick / 10; // in deg |
667 | NaviData.AngleRoll = FromFlightCtrl.AngleRoll / 10; // in deg |
673 | NaviData.AngleRoll = FromFlightCtrl.AngleRoll / 10; // in deg |
668 | NaviData.RC_Quality = (u8)FC.RC_Quality; |
674 | NaviData.RC_Quality = (u8)FC.RC_Quality; |
669 | NaviData.MKFlags = (u8)FC.MKFlags; |
675 | NaviData.MKFlags = (u8)FC.MKFlags; |
670 | NaviData.NCFlags = NCFlags; |
676 | NaviData.NCFlags = NCFlags; |
671 | NaviData.OperatingRadius = Parameter.NaviOperatingRadius; |
677 | NaviData.OperatingRadius = Parameter.NaviOperatingRadius; |
672 | NaviData.TopSpeed = (s16)GPSData.Speed_Top; // in cm/s |
678 | NaviData.TopSpeed = (s16)GPSData.Speed_Top; // in cm/s |
673 | NaviData.TargetHoldTime = (u8)(GetDelay(WPTime)/1000); // in s |
679 | NaviData.TargetHoldTime = (u8)(GetDelay(WPTime)/1000); // in s |
674 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
680 | //+++++++++++++++++++++++++++++++++++++++++++++++++++ |
675 | return; |
681 | return; |
676 | } |
682 | } |
677 | 683 | ||
678 | 684 |