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Line 49... | Line 49... | ||
49 | // + POSSIBILITY OF SUCH DAMAGE. |
49 | // + POSSIBILITY OF SUCH DAMAGE. |
50 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
50 | // ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ |
51 | #include <inttypes.h> |
51 | #include <inttypes.h> |
52 | #include <stdlib.h> |
52 | #include <stdlib.h> |
53 | #include "ubx.h" |
53 | #include "ubx.h" |
54 | #include "mymath.h" |
54 | //#include "mymath.h" |
55 | #include "timer0.h" |
55 | #include "timer0.h" |
56 | #include "uart0.h" |
56 | #include "uart0.h" |
57 | #include "rc.h" |
57 | #include "rc.h" |
58 | #include "eeprom.h" |
58 | #include "eeprom.h" |
Line 85... | Line 85... | ||
85 | // the current flight mode |
85 | // the current flight mode |
86 | FlightMode_t FlightMode = GPS_FLIGHT_MODE_UNDEF; |
86 | FlightMode_t FlightMode = GPS_FLIGHT_MODE_UNDEF; |
Line 87... | Line 87... | ||
87 | 87 | ||
88 | 88 | ||
89 | // --------------------------------------------------------------------------------- |
- | |
90 | void GPS_UpdateParameter(void) |
89 | // --------------------------------------------------------------------------------- |
Line 91... | Line 90... | ||
91 | { |
90 | void GPS_UpdateParameter(void) { |
92 | static FlightMode_t FlightModeOld = GPS_FLIGHT_MODE_UNDEF; |
- | |
93 | 91 | static FlightMode_t FlightModeOld = GPS_FLIGHT_MODE_UNDEF; |
|
94 | if((RC_Quality < 100) || (MKFlags & MKFLAG_EMERGENCY_LANDING)) |
- | |
95 | { |
92 | |
96 | FlightMode = GPS_FLIGHT_MODE_FREE; |
- | |
97 | } |
93 | if((RC_Quality < 100) || (MKFlags & MKFLAG_EMERGENCY_LANDING)) { |
98 | else |
94 | FlightMode = GPS_FLIGHT_MODE_FREE; |
99 | { |
95 | } else { |
100 | if (dynamicParams.NaviGpsModeControl < 50) FlightMode = GPS_FLIGHT_MODE_AID; |
96 | if (dynamicParams.NaviGpsModeControl < 50) FlightMode = GPS_FLIGHT_MODE_AID; |
- | 97 | else if(dynamicParams.NaviGpsModeControl < 180) FlightMode = GPS_FLIGHT_MODE_FREE; |
|
101 | else if(dynamicParams.NaviGpsModeControl < 180) FlightMode = GPS_FLIGHT_MODE_FREE; |
98 | else FlightMode = GPS_FLIGHT_MODE_HOME; |
102 | else FlightMode = GPS_FLIGHT_MODE_HOME; |
- | |
103 | } |
99 | } |
104 | if (FlightMode != FlightModeOld) |
100 | |
105 | { |
101 | if (FlightMode != FlightModeOld) { |
106 | BeepTime = 100; |
102 | BeepTime = 100; |
Line 107... | Line -... | ||
107 | } |
- | |
108 | FlightModeOld = FlightMode; |
- | |
109 | } |
103 | } |
110 | 104 | FlightModeOld = FlightMode; |
|
111 | 105 | } |
|
112 | - | ||
113 | // --------------------------------------------------------------------------------- |
106 | |
114 | // This function defines a good GPS signal condition |
107 | // --------------------------------------------------------------------------------- |
115 | uint8_t GPS_IsSignalOK(void) |
- | |
116 | { |
108 | // This function defines a good GPS signal condition |
117 | static uint8_t GPSFix = 0; |
109 | uint8_t GPS_IsSignalOK(void) { |
118 | if( (GPSInfo.status != INVALID) && (GPSInfo.satfix == SATFIX_3D) && (GPSInfo.flags & FLAG_GPSFIXOK) && ((GPSInfo.satnum >= staticParams.NaviGpsMinSat) || GPSFix)) |
- | |
119 | { |
110 | static uint8_t GPSFix = 0; |
120 | GPSFix = 1; |
111 | if( (GPSInfo.status != INVALID) && (GPSInfo.satfix == SATFIX_3D) && (GPSInfo.flags & FLAG_GPSFIXOK) && ((GPSInfo.satnum >= staticParams.NaviGpsMinSat) || GPSFix)) { |
121 | return(1); |
- | |
122 | 112 | GPSFix = 1; |
|
- | 113 | return 1; |
|
123 | } |
114 | } |
124 | else return (0); |
115 | else return (0); |
125 | 116 | } |
|
126 | } |
- | |
127 | // --------------------------------------------------------------------------------- |
117 | |
128 | // rescale xy-vector length to limit |
118 | // --------------------------------------------------------------------------------- |
129 | uint8_t GPS_LimitXY(int32_t *x, int32_t *y, int32_t limit) |
119 | // rescale xy-vector length to limit |
130 | { |
120 | uint8_t GPS_LimitXY(int32_t *x, int32_t *y, int32_t limit) { |
131 | uint8_t retval = 0; |
- | |
132 | int32_t len; |
121 | uint8_t retval = 0; |
133 | len = (int32_t)c_sqrt(*x * *x + *y * *y); |
122 | int32_t len; |
134 | if (len > limit) |
123 | len = (int32_t)c_sqrt(*x * *x + *y * *y); |
135 | { |
124 | if (len > limit) { |
136 | // normalize control vector components to the limit |
125 | // normalize control vector components to the limit |
137 | *x = (*x * limit) / len; |
126 | *x = (*x * limit) / len; |
138 | *y = (*y * limit) / len; |
127 | *y = (*y * limit) / len; |
Line 139... | Line 128... | ||
139 | retval = 1; |
128 | retval = 1; |
140 | } |
129 | } |
141 | return(retval); |
- | |
142 | } |
130 | return(retval); |
143 | 131 | } |
|
144 | // checks nick and roll sticks for manual control |
132 | |
Line 145... | Line 133... | ||
145 | uint8_t GPS_IsManualControlled(void) |
133 | // checks nick and roll sticks for manual control |
146 | { |
134 | uint8_t GPS_IsManualControlled(void) { |
147 | if ( (abs(PPM_in[staticParams.ChannelAssignment[CH_NICK]]) < staticParams.NaviStickThreshold) && (abs(PPM_in[staticParams.ChannelAssignment[CH_ROLL]]) < staticParams.NaviStickThreshold)) return 0; |
- | |
148 | else return 1; |
135 | if ((abs(PPM_in[staticParams.ChannelAssignment[CH_NICK]]) < staticParams.NaviStickThreshold) && (abs(PPM_in[staticParams.ChannelAssignment[CH_ROLL]]) < staticParams.NaviStickThreshold)) return 0; |
149 | } |
136 | else return 1; |
Line 150... | Line -... | ||
150 | - | ||
151 | // set given position to current gps position |
137 | } |
152 | uint8_t GPS_SetCurrPosition(GPS_Pos_t * pGPSPos) |
138 | |
153 | { |
139 | // set given position to current gps position |
154 | uint8_t retval = 0; |
140 | uint8_t GPS_SetCurrPosition(GPS_Pos_t * pGPSPos) { |
155 | if(pGPSPos == NULL) return(retval); // bad pointer |
141 | uint8_t retval = 0; |
156 | 142 | if(pGPSPos == NULL) return(retval); // bad pointer |
|
157 | if(GPS_IsSignalOK()) |
- | |
158 | { // is GPS signal condition is fine |
- | |
159 | pGPSPos->Longitude = GPSInfo.longitude; |
143 | |
160 | pGPSPos->Latitude = GPSInfo.latitude; |
144 | if(GPS_IsSignalOK()) { // is GPS signal condition is fine |
161 | pGPSPos->Altitude = GPSInfo.altitude; |
145 | pGPSPos->Longitude = GPSInfo.longitude; |
162 | pGPSPos->Status = NEWDATA; |
146 | pGPSPos->Latitude = GPSInfo.latitude; |
163 | retval = 1; |
147 | pGPSPos->Altitude = GPSInfo.altitude; |
164 | } |
148 | pGPSPos->Status = NEWDATA; |
Line 165... | Line 149... | ||
165 | else |
149 | retval = 1; |
166 | { // bad GPS signal condition |
150 | } else { // bad GPS signal condition |
167 | pGPSPos->Status = INVALID; |
- | |
168 | retval = 0; |
151 | pGPSPos->Status = INVALID; |
- | 152 | retval = 0; |
|
169 | } |
153 | } |
170 | return(retval); |
154 | return(retval); |
171 | } |
- | |
172 | 155 | } |
|
173 | // clear position |
156 | |
174 | uint8_t GPS_ClearPosition(GPS_Pos_t * pGPSPos) |
157 | // clear position |
175 | { |
158 | uint8_t GPS_ClearPosition(GPS_Pos_t * pGPSPos) { |
176 | uint8_t retval = 0; |
159 | uint8_t retval = 0; |
177 | if(pGPSPos == NULL) return(retval); // bad pointer |
160 | if(pGPSPos == NULL) |
178 | else |
161 | return retval; // bad pointer |
179 | { |
162 | else { |
Line 180... | Line 163... | ||
180 | pGPSPos->Longitude = 0; |
163 | pGPSPos->Longitude = 0; |
181 | pGPSPos->Latitude = 0; |
164 | pGPSPos->Latitude = 0; |
182 | pGPSPos->Altitude = 0; |
- | |
183 | pGPSPos->Status = INVALID; |
165 | pGPSPos->Altitude = 0; |
184 | retval = 1; |
166 | pGPSPos->Status = INVALID; |
185 | } |
167 | retval = 1; |
Line 186... | Line 168... | ||
186 | return (retval); |
168 | } |
187 | } |
169 | return (retval); |
188 | 170 | } |
|
189 | // disable GPS control sticks |
171 | |
190 | void GPS_Neutral(void) |
- | |
191 | { |
172 | // disable GPS control sticks |
192 | GPSStickNick = 0; |
173 | void GPS_Neutral(void) { |
193 | GPSStickRoll = 0; |
174 | GPSStickNick = 0; |
194 | } |
175 | GPSStickRoll = 0; |
195 | 176 | } |
|
196 | // calculates the GPS control stick values from the deviation to target position |
177 | |
197 | // if the pointer to the target positin is NULL or is the target position invalid |
178 | // calculates the GPS control stick values from the deviation to target position |
198 | // then the P part of the controller is deactivated. |
179 | // if the pointer to the target positin is NULL or is the target position invalid |
Line 199... | Line 180... | ||
199 | void GPS_PIDController(GPS_Pos_t *pTargetPos) |
180 | // then the P part of the controller is deactivated. |
200 | { |
181 | void GPS_PIDController(GPS_Pos_t *pTargetPos) { |
201 | static int32_t PID_Nick, PID_Roll; |
- | |
202 | int32_t coscompass, sincompass; |
- | |
203 | int32_t GPSPosDev_North, GPSPosDev_East; // Position deviation in cm |
182 | static int32_t PID_Nick, PID_Roll; |
204 | int32_t P_North = 0, D_North = 0, P_East = 0, D_East = 0, I_North = 0, I_East = 0; |
183 | int32_t coscompass, sincompass; |
205 | int32_t PID_North = 0, PID_East = 0; |
184 | int32_t GPSPosDev_North, GPSPosDev_East; // Position deviation in cm |
206 | static int32_t cos_target_latitude = 1; |
185 | int32_t P_North = 0, D_North = 0, P_East = 0, D_East = 0, I_North = 0, I_East = 0; |
207 | static int32_t GPSPosDevIntegral_North = 0, GPSPosDevIntegral_East = 0; |
186 | int32_t PID_North = 0, PID_East = 0; |
Line 267... | Line 246... | ||
267 | 246 | ||
268 | // I-Part |
247 | // I-Part |
269 | I_North = ((int32_t)dynamicParams.NaviGpsI * GPSPosDevIntegral_North)/8192; |
248 | I_North = ((int32_t)dynamicParams.NaviGpsI * GPSPosDevIntegral_North)/8192; |
Line 270... | Line -... | ||
270 | I_East = ((int32_t)dynamicParams.NaviGpsI * GPSPosDevIntegral_East)/8192; |
- | |
271 | 249 | I_East = ((int32_t)dynamicParams.NaviGpsI * GPSPosDevIntegral_East)/8192; |
|
272 | 250 | ||
273 | // combine P & I |
251 | // combine P & I |
274 | PID_North = P_North + I_North; |
252 | PID_North = P_North + I_North; |
275 | PID_East = P_East + I_East; |
253 | PID_East = P_East + I_East; |
Line 282... | Line 260... | ||
282 | 260 | ||
283 | // combine PI- and D-Part |
261 | // combine PI- and D-Part |
284 | PID_North += D_North; |
262 | PID_North += D_North; |
Line 285... | Line -... | ||
285 | PID_East += D_East; |
- | |
286 | 263 | PID_East += D_East; |
|
287 | 264 | ||
288 | // scale combination with gain. |
265 | // scale combination with gain. |
Line 289... | Line 266... | ||
289 | PID_North = (PID_North * (int32_t)dynamicParams.NaviGpsGain) / 100; |
266 | PID_North = (PID_North * (int32_t)dynamicParams.NaviGpsGain) / 100; |
290 | PID_East = (PID_East * (int32_t)dynamicParams.NaviGpsGain) / 100; |
- | |
291 | 267 | PID_East = (PID_East * (int32_t)dynamicParams.NaviGpsGain) / 100; |
|
292 | // GPS to nick and roll settings |
268 | |
293 | 269 | // GPS to nick and roll settings |
|
294 | // A positive nick angle moves head downwards (flying forward). |
270 | // A positive nick angle moves head downwards (flying forward). |
295 | // A positive roll angle tilts left side downwards (flying left). |
271 | // A positive roll angle tilts left side downwards (flying left). |
Line 306... | Line 282... | ||
306 | coscompass = (int32_t)c_cos_8192(YawGyroHeading / GYRO_DEG_FACTOR); |
282 | coscompass = (int32_t)c_cos_8192(YawGyroHeading / GYRO_DEG_FACTOR); |
307 | sincompass = (int32_t)c_sin_8192(YawGyroHeading / GYRO_DEG_FACTOR); |
283 | sincompass = (int32_t)c_sin_8192(YawGyroHeading / GYRO_DEG_FACTOR); |
308 | PID_Nick = (coscompass * PID_North + sincompass * PID_East) / 8192; |
284 | PID_Nick = (coscompass * PID_North + sincompass * PID_East) / 8192; |
309 | PID_Roll = (sincompass * PID_North - coscompass * PID_East) / 8192; |
285 | PID_Roll = (sincompass * PID_North - coscompass * PID_East) / 8192; |
Line 310... | Line -... | ||
310 | - | ||
311 | 286 | ||
312 | // limit resulting GPS control vector |
287 | // limit resulting GPS control vector |
Line 313... | Line 288... | ||
313 | GPS_LimitXY(&PID_Nick, &PID_Roll, GPS_STICK_LIMIT); |
288 | GPS_LimitXY(&PID_Nick, &PID_Roll, GPS_STICK_LIMIT); |
314 | 289 | ||
Line 322... | Line 297... | ||
322 | GPSPosDevIntegral_North = 0; |
297 | GPSPosDevIntegral_North = 0; |
323 | GPSPosDevIntegral_East = 0; |
298 | GPSPosDevIntegral_East = 0; |
324 | } |
299 | } |
325 | } |
300 | } |
Line 326... | Line -... | ||
326 | - | ||
327 | - | ||
328 | - | ||
329 | 301 | ||
330 | void GPS_Main(void) |
- | |
331 | { |
302 | void GPS_Main(void) { |
332 | static uint8_t GPS_P_Delay = 0; |
303 | static uint8_t GPS_P_Delay = 0; |
Line 333... | Line 304... | ||
333 | static uint16_t beep_rythm = 0; |
304 | static uint16_t beep_rythm = 0; |
Line 334... | Line 305... | ||
334 | 305 | ||
335 | GPS_UpdateParameter(); |
306 | GPS_UpdateParameter(); |
336 | - | ||
337 | // store home position if start of flight flag is set |
307 | |
338 | if(MKFlags & MKFLAG_CALIBRATE) |
308 | // store home position if start of flight flag is set |
Line 339... | Line 309... | ||
339 | { |
309 | if(MKFlags & MKFLAG_CALIBRATE) { |
340 | if(GPS_SetCurrPosition(&HomePosition)) BeepTime = 700; |
- | |
341 | } |
310 | if(GPS_SetCurrPosition(&HomePosition)) BeepTime = 700; |
342 | 311 | } |
|
343 | switch(GPSInfo.status) |
312 | |
344 | { |
- | |
345 | case INVALID: // invalid gps data |
313 | switch(GPSInfo.status) { |
346 | GPS_Neutral(); |
314 | case INVALID: // invalid gps data |
347 | if(FlightMode != GPS_FLIGHT_MODE_FREE) |
315 | GPS_Neutral(); |
348 | { |
316 | if(FlightMode != GPS_FLIGHT_MODE_FREE) { |
349 | BeepTime = 100; // beep if signal is neccesary |
317 | BeepTime = 100; // beep if signal is neccesary |