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Rev | Author | Line No. | Line |
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726 | killagreg | 1 | #include <inttypes.h> |
764 | killagreg | 2 | #include <stdlib.h> |
726 | killagreg | 3 | #include "fc.h" |
4 | #include "ubx.h" |
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5 | #include "mymath.h" |
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727 | killagreg | 6 | #include "timer0.h" |
741 | killagreg | 7 | #include "uart.h" |
794 | killagreg | 8 | #include "rc.h" |
9 | #include "eeprom.h" |
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701 | killagreg | 10 | |
741 | killagreg | 11 | #define TSK_IDLE 0 |
12 | #define TSK_HOLD 1 |
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13 | #define TSK_HOME 2 |
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14 | |||
844 | killagreg | 15 | #define GPS_STICK_SENSE 15 // must be at least in a range where 90% of the trimming does not switch of the GPS function |
16 | #define GPS_STICK_LIMIT 35 // limit of gps stick control to avoid critical flight attitudes |
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812 | killagreg | 17 | #define GPS_POSDEV_INTEGRAL_LIMIT 32000 // limit for the position error integral |
844 | killagreg | 18 | #define MAX_VELOCITY 700 // max ground speed in cm/s during position control |
741 | killagreg | 19 | |
726 | killagreg | 20 | |
812 | killagreg | 21 | int16_t GPS_Pitch = 0, GPS_Roll = 0; |
844 | killagreg | 22 | uint8_t GPS_P_Factor = 0, GPS_I_Factor = 0, GPS_D_Factor = 0; |
726 | killagreg | 23 | |
746 | killagreg | 24 | |
781 | killagreg | 25 | |
726 | killagreg | 26 | typedef struct |
1 | ingob | 27 | { |
781 | killagreg | 28 | int32_t Longitude; |
29 | int32_t Latitude; |
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794 | killagreg | 30 | int32_t Altitude; |
726 | killagreg | 31 | uint8_t Status; |
32 | } GPS_Pos_t; |
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33 | |||
34 | // GPS coordinates for hold position |
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794 | killagreg | 35 | GPS_Pos_t HoldPosition = {0,0,0,INVALID}; |
741 | killagreg | 36 | // GPS coordinates for home position |
794 | killagreg | 37 | GPS_Pos_t HomePosition = {0,0,0,INVALID}; |
726 | killagreg | 38 | |
39 | |||
40 | // --------------------------------------------------------------------------------- |
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41 | |||
794 | killagreg | 42 | // checks pitch and roll sticks for manual control |
43 | uint8_t IsManualControlled(void) |
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44 | { |
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45 | if ( (abs(PPM_in[ParamSet.ChannelAssignment[CH_PITCH]]) < GPS_STICK_SENSE) && (abs(PPM_in[ParamSet.ChannelAssignment[CH_ROLL]]) < GPS_STICK_SENSE)) return 0; |
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46 | else return 1; |
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47 | } |
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48 | |||
781 | killagreg | 49 | // set home position to current positon |
746 | killagreg | 50 | void GPS_SetHomePosition(void) |
51 | { |
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781 | killagreg | 52 | if( ((GPSInfo.status == VALID) || (GPSInfo.status == PROCESSED)) && GPSInfo.satfix == SATFIX_3D) |
53 | { |
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54 | HomePosition.Longitude = GPSInfo.longitude; |
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55 | HomePosition.Latitude = GPSInfo.latitude; |
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794 | killagreg | 56 | HomePosition.Altitude = GPSInfo.altitude; |
781 | killagreg | 57 | HomePosition.Status = VALID; |
58 | BeepTime = 1000; // signal if new home position was set |
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59 | } |
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60 | else |
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61 | { |
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62 | HomePosition.Status = INVALID; |
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63 | } |
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746 | killagreg | 64 | } |
726 | killagreg | 65 | |
781 | killagreg | 66 | // set hold position to current positon |
67 | void GPS_SetHoldPosition(void) |
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68 | { |
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69 | if( ((GPSInfo.status == VALID) || (GPSInfo.status == PROCESSED)) && GPSInfo.satfix == SATFIX_3D) |
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70 | { |
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71 | HoldPosition.Longitude = GPSInfo.longitude; |
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72 | HoldPosition.Latitude = GPSInfo.latitude; |
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794 | killagreg | 73 | HoldPosition.Altitude = GPSInfo.altitude; |
781 | killagreg | 74 | HoldPosition.Status = VALID; |
75 | } |
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76 | else |
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77 | { |
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78 | HoldPosition.Status = INVALID; |
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79 | } |
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80 | } |
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81 | |||
762 | killagreg | 82 | // clear home position |
83 | void GPS_ClearHomePosition(void) |
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84 | { |
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85 | HomePosition.Status = INVALID; |
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86 | } |
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746 | killagreg | 87 | |
747 | killagreg | 88 | // disable GPS control sticks |
746 | killagreg | 89 | void GPS_Neutral(void) |
1 | ingob | 90 | { |
746 | killagreg | 91 | GPS_Pitch = 0; |
92 | GPS_Roll = 0; |
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93 | } |
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94 | |||
792 | killagreg | 95 | // calculates the GPS control stick values from the deviation to target position |
96 | // if the pointer to the target positin is NULL or is the target position invalid |
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97 | // then the P part of the controller is deactivated. |
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812 | killagreg | 98 | void GPS_PIDController(GPS_Pos_t *pTargetPos) |
746 | killagreg | 99 | { |
829 | killagreg | 100 | int32_t temp, temp1, PID_Pitch, PID_Roll; |
726 | killagreg | 101 | int32_t coscompass, sincompass; |
781 | killagreg | 102 | int32_t GPSPosDev_North, GPSPosDev_East; // Position deviation in cm |
812 | killagreg | 103 | int32_t P_North = 0, D_North = 0, P_East = 0, D_East = 0, I_North = 0, I_East = 0; |
104 | int32_t PID_North = 0, PID_East = 0; |
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781 | killagreg | 105 | static int32_t cos_target_latitude = 1; |
812 | killagreg | 106 | static int32_t GPSPosDevIntegral_North = 0, GPSPosDevIntegral_East = 0; |
107 | static GPS_Pos_t *pLastTargetPos = 0; |
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746 | killagreg | 108 | |
792 | killagreg | 109 | // if GPS data and Compass are ok |
110 | if((GPSInfo.status == VALID) && (GPSInfo.satfix == SATFIX_3D) && (CompassHeading >= 0) ) |
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111 | { |
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781 | killagreg | 112 | |
792 | killagreg | 113 | if(pTargetPos != NULL) // if there is a target position |
781 | killagreg | 114 | { |
792 | killagreg | 115 | if(pTargetPos->Status != INVALID) // and the position data are valid |
812 | killagreg | 116 | { |
117 | // if the target data are updated or the target pointer has changed |
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118 | if ((pTargetPos->Status != PROCESSED) || (pTargetPos != pLastTargetPos) ) |
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792 | killagreg | 119 | { |
812 | killagreg | 120 | // reset error integral |
121 | GPSPosDevIntegral_North = 0; |
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122 | GPSPosDevIntegral_East = 0; |
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123 | // recalculate latitude projection |
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792 | killagreg | 124 | cos_target_latitude = (int32_t)c_cos_8192((int16_t)(pTargetPos->Latitude/10000000L)); |
812 | killagreg | 125 | // remember last target pointer |
126 | pLastTargetPos = pTargetPos; |
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127 | // mark data as processed |
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792 | killagreg | 128 | pTargetPos->Status = PROCESSED; |
129 | } |
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812 | killagreg | 130 | // calculate position deviation from latitude and longitude differences |
131 | GPSPosDev_North = (GPSInfo.latitude - pTargetPos->Latitude); // to calculate real cm we would need *111/100 additionally |
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132 | GPSPosDev_East = (GPSInfo.longitude - pTargetPos->Longitude); // to calculate real cm we would need *111/100 additionally |
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792 | killagreg | 133 | // calculate latitude projection |
134 | GPSPosDev_East *= cos_target_latitude; |
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135 | GPSPosDev_East /= 8192; |
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746 | killagreg | 136 | |
812 | killagreg | 137 | DebugOut.Analog[12] = GPSPosDev_North; |
792 | killagreg | 138 | DebugOut.Analog[13] = GPSPosDev_East; |
139 | //DebugOut.Analog[12] = GPSInfo.velnorth; |
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140 | //DebugOut.Analog[13] = GPSInfo.veleast; |
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141 | } |
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812 | killagreg | 142 | else // no valid target position available |
792 | killagreg | 143 | { |
812 | killagreg | 144 | // reset error |
792 | killagreg | 145 | GPSPosDev_North = 0; |
146 | GPSPosDev_East = 0; |
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812 | killagreg | 147 | // reset error integral |
148 | GPSPosDevIntegral_North = 0; |
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149 | GPSPosDevIntegral_East = 0; |
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792 | killagreg | 150 | } |
151 | } |
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812 | killagreg | 152 | else // no target position available |
792 | killagreg | 153 | { |
812 | killagreg | 154 | // reset error |
792 | killagreg | 155 | GPSPosDev_North = 0; |
156 | GPSPosDev_East = 0; |
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812 | killagreg | 157 | // reset error integral |
158 | GPSPosDevIntegral_North = 0; |
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159 | GPSPosDevIntegral_East = 0; |
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792 | killagreg | 160 | } |
767 | killagreg | 161 | |
812 | killagreg | 162 | //Calculate PID-components of the controller (negative sign for compensation) |
829 | killagreg | 163 | |
164 | // P-Part |
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844 | killagreg | 165 | P_North = -((int32_t)GPS_P_Factor * GPSPosDev_North)/2048; |
166 | P_East = -((int32_t)GPS_P_Factor * GPSPosDev_East)/2048; |
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829 | killagreg | 167 | |
830 | killagreg | 168 | // I-Part |
844 | killagreg | 169 | I_North = -((int32_t)GPS_I_Factor * GPSPosDevIntegral_North)/8192; |
170 | I_East = -((int32_t)GPS_I_Factor * GPSPosDevIntegral_East)/8192; |
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830 | killagreg | 171 | |
172 | // combine P- & I-Part |
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173 | PID_North = P_North + I_North; |
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174 | PID_East = P_East + I_East; |
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175 | |||
176 | //limit PI-Part to limit the max velocity |
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844 | killagreg | 177 | temp1 = ((int32_t)GPS_D_Factor * MAX_VELOCITY)/512; // the PI-Part limit |
830 | killagreg | 178 | temp = (int32_t)c_sqrt(PID_North*PID_North + PID_East*PID_East); // the current PI-Part |
829 | killagreg | 179 | if(temp > temp1) // P-Part limit is reached |
180 | { |
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181 | // normalize P-part components to the P-Part limit |
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830 | killagreg | 182 | PID_North = (PID_North * temp1)/temp; |
844 | killagreg | 183 | PID_East = (PID_East * temp1) /temp; |
829 | killagreg | 184 | } |
830 | killagreg | 185 | else // PI-Part under its limit |
829 | killagreg | 186 | { |
830 | killagreg | 187 | // update position error integrals |
829 | killagreg | 188 | GPSPosDevIntegral_North += GPSPosDev_North/16; |
189 | if( GPSPosDevIntegral_North > GPS_POSDEV_INTEGRAL_LIMIT) GPSPosDevIntegral_North = GPS_POSDEV_INTEGRAL_LIMIT; |
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190 | else if (GPSPosDevIntegral_North < -GPS_POSDEV_INTEGRAL_LIMIT) GPSPosDevIntegral_North = -GPS_POSDEV_INTEGRAL_LIMIT; |
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191 | GPSPosDevIntegral_East += GPSPosDev_East/16; |
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192 | if( GPSPosDevIntegral_East > GPS_POSDEV_INTEGRAL_LIMIT) GPSPosDevIntegral_East = GPS_POSDEV_INTEGRAL_LIMIT; |
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193 | else if (GPSPosDevIntegral_East < -GPS_POSDEV_INTEGRAL_LIMIT) GPSPosDevIntegral_East = -GPS_POSDEV_INTEGRAL_LIMIT; |
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194 | } |
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195 | |||
830 | killagreg | 196 | // D-Part |
844 | killagreg | 197 | D_North = -((int32_t)GPS_D_Factor * GPSInfo.velnorth)/512; |
198 | D_East = -((int32_t)GPS_D_Factor * GPSInfo.veleast)/512; |
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829 | killagreg | 199 | |
200 | |||
830 | killagreg | 201 | // combine PI- and D-Part |
202 | PID_North += D_North; |
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203 | PID_East += D_East; |
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746 | killagreg | 204 | |
762 | killagreg | 205 | // GPS to pitch and roll settings |
746 | killagreg | 206 | |
792 | killagreg | 207 | // A positive pitch angle moves head downwards (flying forward). |
208 | // A positive roll angle tilts left side downwards (flying left). |
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762 | killagreg | 209 | // If compass heading is 0 the head of the copter is in north direction. |
210 | // A positive pitch angle will fly to north and a positive roll angle will fly to west. |
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211 | // In case of a positive north deviation/velocity the |
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212 | // copter should fly to south (negative pitch). |
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213 | // In case of a positive east position deviation and a positive east velocity the |
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214 | // copter should fly to west (positive roll). |
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215 | // The influence of the GPS_Pitch and GPS_Roll variable is contrarily to the stick values |
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216 | // in the fc.c. Therefore a positive north deviation/velocity should result in a positive |
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217 | // GPS_Pitch and a positive east deviation/velocity should result in a negative GPS_Roll. |
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218 | |||
792 | killagreg | 219 | coscompass = (int32_t)c_cos_8192(CompassHeading); |
220 | sincompass = (int32_t)c_sin_8192(CompassHeading); |
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828 | killagreg | 221 | PID_Roll = (coscompass * PID_East - sincompass * PID_North) / 8192; |
222 | PID_Pitch = -1*((sincompass * PID_East + coscompass * PID_North) / 8192); |
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792 | killagreg | 223 | |
829 | killagreg | 224 | // limit resulting GPS control vector |
225 | temp = (int32_t)c_sqrt(PID_Roll*PID_Roll + PID_Pitch*PID_Pitch); |
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226 | if (temp > GPS_STICK_LIMIT) |
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812 | killagreg | 227 | { |
828 | killagreg | 228 | // normalize control vector components to the limit |
829 | killagreg | 229 | PID_Roll = (PID_Roll * GPS_STICK_LIMIT)/temp; |
230 | PID_Pitch = (PID_Pitch * GPS_STICK_LIMIT)/temp; |
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812 | killagreg | 231 | } |
232 | |||
828 | killagreg | 233 | GPS_Roll = (int16_t)PID_Roll; |
234 | GPS_Pitch = (int16_t)PID_Pitch; |
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235 | |||
746 | killagreg | 236 | } |
818 | killagreg | 237 | else // invalid GPS data or bad compass reading |
746 | killagreg | 238 | { |
792 | killagreg | 239 | GPS_Neutral(); // do nothing |
812 | killagreg | 240 | // reset error integral |
241 | GPSPosDevIntegral_North = 0; |
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242 | GPSPosDevIntegral_East = 0; |
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746 | killagreg | 243 | } |
244 | } |
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245 | |||
246 | |||
812 | killagreg | 247 | |
248 | |||
762 | killagreg | 249 | void GPS_Main(uint8_t ctrl) |
746 | killagreg | 250 | { |
741 | killagreg | 251 | static uint8_t GPS_Task = TSK_IDLE; |
792 | killagreg | 252 | static uint8_t GPS_P_Delay = 0; |
752 | killagreg | 253 | int16_t satbeep; |
1 | ingob | 254 | |
762 | killagreg | 255 | // ctrl enables the gps feature |
256 | if(ctrl < 70) GPS_Task = TSK_IDLE; |
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257 | else if (ctrl < 160) GPS_Task = TSK_HOLD; |
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258 | else GPS_Task = TSK_HOME; // ctrl >= 160 |
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741 | killagreg | 259 | |
260 | |||
261 | switch(GPSInfo.status) |
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726 | killagreg | 262 | { |
741 | killagreg | 263 | case INVALID: // invalid gps data |
746 | killagreg | 264 | GPS_Neutral(); |
752 | killagreg | 265 | if(GPS_Task != TSK_IDLE) |
266 | { |
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267 | BeepTime = 100; // beep if signal is neccesary |
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268 | } |
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741 | killagreg | 269 | break; |
781 | killagreg | 270 | case PROCESSED: // if gps data are already processed do nothing |
741 | killagreg | 271 | // downcount timeout |
272 | if(GPSTimeout) GPSTimeout--; |
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273 | // if no new data arrived within timeout set current data invalid |
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274 | // and therefore disable GPS |
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275 | else |
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726 | killagreg | 276 | { |
746 | killagreg | 277 | GPS_Neutral(); |
741 | killagreg | 278 | GPSInfo.status = INVALID; |
279 | } |
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280 | break; |
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281 | case VALID: // new valid data from gps device |
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781 | killagreg | 282 | // if the gps data quality is good |
741 | killagreg | 283 | if (GPSInfo.satfix == SATFIX_3D) |
284 | { |
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285 | switch(GPS_Task) // check what's to do |
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726 | killagreg | 286 | { |
741 | killagreg | 287 | case TSK_IDLE: |
781 | killagreg | 288 | // update hold position to current gps position |
289 | GPS_SetHoldPosition(); // can get invalid if gps signal is bad |
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741 | killagreg | 290 | // disable gps control |
746 | killagreg | 291 | GPS_Neutral(); |
741 | killagreg | 292 | break; // eof TSK_IDLE |
293 | case TSK_HOLD: |
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781 | killagreg | 294 | if(HoldPosition.Status != INVALID) |
741 | killagreg | 295 | { |
794 | killagreg | 296 | if( IsManualControlled() ) // MK controlled by user |
762 | killagreg | 297 | { |
794 | killagreg | 298 | // update hold point to current gps position |
299 | GPS_SetHoldPosition(); |
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300 | // disable gps control |
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301 | GPS_Neutral(); |
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302 | GPS_P_Delay = 0; |
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303 | } |
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304 | else // GPS control active |
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305 | { |
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792 | killagreg | 306 | if(GPS_P_Delay<7) |
307 | { // delayed activation of P-Part for 8 cycles (8*0.25s = 2s) |
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308 | GPS_P_Delay++; |
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309 | GPS_SetHoldPosition(); // update hold point to current gps position |
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812 | killagreg | 310 | GPS_PIDController(NULL); // activates only the D-Part |
792 | killagreg | 311 | } |
812 | killagreg | 312 | else GPS_PIDController(&HoldPosition);// activates the P&D-Part |
762 | killagreg | 313 | } |
741 | killagreg | 314 | } |
781 | killagreg | 315 | else // invalid Hold Position |
316 | { // try to catch a valid hold position from gps data input |
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317 | GPS_SetHoldPosition(); |
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318 | GPS_Neutral(); |
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319 | } |
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741 | killagreg | 320 | break; // eof TSK_HOLD |
746 | killagreg | 321 | case TSK_HOME: |
781 | killagreg | 322 | if(HomePosition.Status != INVALID) |
746 | killagreg | 323 | { |
324 | // update hold point to current gps position |
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762 | killagreg | 325 | // to avoid a flight back if home comming is deactivated |
781 | killagreg | 326 | GPS_SetHoldPosition(); |
794 | killagreg | 327 | if( IsManualControlled() ) // MK controlled by user |
762 | killagreg | 328 | { |
794 | killagreg | 329 | GPS_Neutral(); |
762 | killagreg | 330 | } |
794 | killagreg | 331 | else // GPS control active |
767 | killagreg | 332 | { |
812 | killagreg | 333 | GPS_PIDController(&HomePosition); |
767 | killagreg | 334 | } |
746 | killagreg | 335 | } |
336 | else // bad home position |
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337 | { |
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338 | BeepTime = 50; // signal invalid home position |
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762 | killagreg | 339 | // try to hold at least the position as a fallback option |
781 | killagreg | 340 | |
341 | if (HoldPosition.Status != INVALID) |
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762 | killagreg | 342 | { |
794 | killagreg | 343 | if( IsManualControlled() ) // MK controlled by user |
781 | killagreg | 344 | { |
794 | killagreg | 345 | GPS_Neutral(); |
781 | killagreg | 346 | } |
794 | killagreg | 347 | else // GPS control active |
781 | killagreg | 348 | { |
812 | killagreg | 349 | GPS_PIDController(&HoldPosition); |
781 | killagreg | 350 | } |
762 | killagreg | 351 | } |
781 | killagreg | 352 | else |
353 | { // try to catch a valid hold position |
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354 | GPS_SetHoldPosition(); |
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767 | killagreg | 355 | GPS_Neutral(); |
356 | } |
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746 | killagreg | 357 | } |
358 | break; // eof TSK_HOME |
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741 | killagreg | 359 | default: // unhandled task |
746 | killagreg | 360 | GPS_Neutral(); |
741 | killagreg | 361 | break; // eof default |
362 | } // eof switch GPS_Task |
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363 | } // eof 3D-FIX |
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364 | else // no 3D-SATFIX |
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365 | { // disable gps control |
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746 | killagreg | 366 | GPS_Neutral(); |
752 | killagreg | 367 | if(GPS_Task != TSK_IDLE) |
368 | { |
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806 | killagreg | 369 | satbeep = 1600 - (int16_t)GPSInfo.satnum * 200; // is zero at 8 sats |
752 | killagreg | 370 | if (satbeep < 0) satbeep = 0; |
806 | killagreg | 371 | BeepTime = 50 + (uint16_t)satbeep; // max 1650 * 0.1 ms = |
752 | killagreg | 372 | } |
741 | killagreg | 373 | } |
374 | // set current data as processed to avoid further calculations on the same gps data |
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375 | GPSInfo.status = PROCESSED; |
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376 | break; |
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377 | } // eof GPSInfo.status |
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378 | DebugOut.Analog[14] = GPS_Pitch; |
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379 | DebugOut.Analog[15] = GPS_Roll; |
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726 | killagreg | 380 | } |
381 |