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1 | /* |
1 | /* |
Line 2... | Line 2... | ||
2 | 2 | ||
Line 3... | Line 3... | ||
3 | Copyright 2007, Niklas Nold |
3 | Copyright 2008, by Killagreg |
4 | 4 | ||
5 | This program (files compass.c and compass.h) is free software; you can redistribute it and/or modify |
5 | This program (files mm3.c and mm3.h) is free software; you can redistribute it and/or modify |
6 | it under the terms of the GNU Lesser General Public License as published by the Free Software Foundation; |
6 | it under the terms of the GNU Lesser General Public License as published by the Free Software Foundation; |
7 | either version 3 of the License, or (at your option) any later version. |
7 | either version 3 of the License, or (at your option) any later version. |
8 | This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; |
8 | This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; |
9 | without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the |
9 | without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the |
Line -... | Line 10... | ||
- | 10 | GNU Lesser General Public License for more details. You should have received a copy of the GNU Lesser General Public License |
|
10 | GNU Lesser General Public License for more details. You should have received a copy of the GNU Lesser General Public License |
11 | along with this program. If not, see <http://www.gnu.org/licenses/>. |
11 | along with this program. If not, see <http://www.gnu.org/licenses/>. |
12 | |
12 | 13 | Please note: The original implementation was done by Niklas Nold. |
|
13 | Please note: All the other files for the project "Mikrokopter" by H. Buss are under the license (license_buss.txt) published by www.mikrokopter.de |
14 | All the other files for the project "Mikrokopter" by H. Buss are under the license (license_buss.txt) published by www.mikrokopter.de |
14 | */ |
15 | */ |
Line 59... | Line 60... | ||
59 | #define MM3_PERIOD_2048 0x60 |
60 | #define MM3_PERIOD_2048 0x60 |
60 | #define MM3_PERIOD_4096 0x70 |
61 | #define MM3_PERIOD_4096 0x70 |
Line 61... | Line 62... | ||
61 | 62 | ||
62 | MM3_calib_t MM3_calib; |
63 | MM3_calib_t MM3_calib; |
- | 64 | volatile MM3_working_t MM3; |
|
Line 63... | Line 65... | ||
63 | volatile MM3_working_t MM3; |
65 | static volatile uint8_t MM3_Timeout = 0; |
64 | 66 | ||
Line 105... | Line 107... | ||
105 | MM3_calib.Z_off = (int8_t)GetParamByte(PID_MM3_Z_OFF); |
107 | MM3_calib.Z_off = (int8_t)GetParamByte(PID_MM3_Z_OFF); |
106 | MM3_calib.X_range = (int16_t)GetParamWord(PID_MM3_X_RANGE); |
108 | MM3_calib.X_range = (int16_t)GetParamWord(PID_MM3_X_RANGE); |
107 | MM3_calib.Y_range = (int16_t)GetParamWord(PID_MM3_Y_RANGE); |
109 | MM3_calib.Y_range = (int16_t)GetParamWord(PID_MM3_Y_RANGE); |
108 | MM3_calib.Z_range = (int16_t)GetParamWord(PID_MM3_Z_RANGE); |
110 | MM3_calib.Z_range = (int16_t)GetParamWord(PID_MM3_Z_RANGE); |
Line -... | Line 111... | ||
- | 111 | ||
- | 112 | MM3_Timeout = 0; |
|
109 | 113 | ||
110 | SREG = sreg; |
114 | SREG = sreg; |
Line 111... | Line 115... | ||
111 | } |
115 | } |
112 | 116 | ||
113 | 117 | ||
114 | /*********************************************/ |
118 | /*********************************************/ |
115 | /* Get Data from MM3 */ |
119 | /* Get Data from MM3 */ |
116 | /*********************************************/ |
120 | /*********************************************/ |
117 | void MM3_Update() // called every 102.4 ms by timer 0 ISR |
121 | void MM3_Update() // called every 102.4 µs by timer 0 ISR |
118 | { |
122 | { |
119 | switch (MM3.STATE) |
123 | switch (MM3.STATE) |
120 | { |
124 | { |
121 | case MM3_STATE_RESET: |
125 | case MM3_STATE_RESET: |
122 | PORTC &= ~(1<<PORTC4); // select slave |
126 | PORTC &= ~(1<<PORTC4); // select slave |
Line 123... | Line 127... | ||
123 | PORTC |= (1<<PORTC5); // PC5 to High, MM3 Reset |
127 | PORTC |= (1<<PORTC5); // PC5 to High, MM3 Reset |
124 | MM3.STATE = MM3_STATE_START_TRANSFER; |
128 | MM3.STATE = MM3_STATE_START_TRANSFER; |
Line 125... | Line 129... | ||
125 | return; |
129 | return; |
126 | 130 | ||
- | 131 | case MM3_STATE_START_TRANSFER: |
|
- | 132 | PORTC &= ~(1<<PORTC5); // PC4 auf Low (was 102.4 µs at high level) |
|
- | 133 | ||
127 | case MM3_STATE_START_TRANSFER: |
134 | // write to SPDR triggers automatically the transfer MOSI MISO |
- | 135 | // MM3 Period, + AXIS code |
|
- | 136 | switch(MM3.AXIS) |
|
128 | PORTC &= ~(1<<PORTC5); // PC4 auf Low (was 102.4 µs at high level) |
137 | { |
- | 138 | case MM3_X_AXIS: |
|
- | 139 | SPDR = MM3_PERIOD_256 + MM3_X_AXIS; |
|
129 | 140 | break; |
|
- | 141 | case MM3_Y_AXIS: |
|
- | 142 | SPDR = MM3_PERIOD_256 + MM3_Y_AXIS; |
|
- | 143 | break; |
|
- | 144 | case MM3_Z_AXIS: |
|
- | 145 | SPDR = MM3_PERIOD_256 + MM3_Z_AXIS; |
|
- | 146 | break; |
|
Line 130... | Line 147... | ||
130 | // write to SPDR triggers automatically the transfer MOSI MISO |
147 | default: |
131 | // MM3 Period, + AXIS code |
148 | MM3.AXIS = MM3_X_AXIS; |
132 | if (MM3.AXIS == MM3_X_AXIS) SPDR = MM3_PERIOD_256 + MM3_X_AXIS; |
149 | MM3.STATE = MM3_STATE_RESET; |
133 | else if (MM3.AXIS == MM3_Y_AXIS) SPDR = MM3_PERIOD_256 + MM3_Y_AXIS; |
150 | return; |
Line 194... | Line 211... | ||
194 | break; |
211 | break; |
195 | } |
212 | } |
196 | } |
213 | } |
197 | PORTC |= (1<<PORTC4); // deselect slave |
214 | PORTC |= (1<<PORTC4); // deselect slave |
198 | MM3.STATE = MM3_STATE_RESET; |
215 | MM3.STATE = MM3_STATE_RESET; |
- | 216 | // Update timeout is called every 102.4 µs. |
|
- | 217 | // It takes 2 cycles to write a measurement data request for one axis and |
|
- | 218 | // at at least 8 ms / 102.4 µs = 79 cycles to read the requested data back. |
|
- | 219 | // I.e. 81 cycles * 102.4 µs = 8.3ms per axis. |
|
- | 220 | // The two function accessing the MM3 Data - MM3_Calibrate() and MM3_Heading() - |
|
- | 221 | // decremtent the MM3_Timeout every 100 ms. |
|
- | 222 | // incrementing the counter by 1 every 8.3 ms is sufficient to avoid a timeout. |
|
- | 223 | if ((MM3.x_axis != MM3.y_axis) || (MM3.x_axis != MM3.z_axis) || (MM3.y_axis != MM3.z_axis)) |
|
- | 224 | { // if all axis measurements give diffrent readings the data should be valid |
|
- | 225 | if(MM3_Timeout < 20) MM3_Timeout++; |
|
- | 226 | } |
|
- | 227 | else // something is very strange here |
|
- | 228 | { |
|
- | 229 | if(MM3_Timeout ) MM3_Timeout--; |
|
- | 230 | } |
|
- | 231 | return; |
|
- | 232 | ||
- | 233 | default: |
|
- | 234 | return; |
|
199 | } |
235 | } |
200 | } |
236 | } |
Line 212... | Line 248... | ||
212 | 248 | ||
213 | GRN_ON; |
249 | GRN_ON; |
Line 214... | Line 250... | ||
214 | ROT_OFF; |
250 | ROT_OFF; |
215 | 251 | ||
216 | // get maximum and minimum reading of all axis |
252 | // get maximum and minimum reading of all axis |
217 | while (measurement) |
253 | while (measurement && !MM3_Timeout) |
218 | { |
254 | { |
Line 219... | Line 255... | ||
219 | if (MM3.x_axis > x_max) x_max = MM3.x_axis; |
255 | if (MM3.x_axis > x_max) x_max = MM3.x_axis; |
Line 231... | Line 267... | ||
231 | GRN_FLASH; |
267 | GRN_FLASH; |
232 | BeepTime = 50; |
268 | BeepTime = 50; |
233 | beeper = 50; |
269 | beeper = 50; |
234 | } |
270 | } |
235 | beeper--; |
271 | beeper--; |
236 | - | ||
237 | // loop with period of 10 ms / 100 Hz |
272 | // loop with period of 10 ms / 100 Hz |
238 | timer = SetDelay(10); |
273 | timer = SetDelay(10); |
239 | while(!CheckDelay(timer)); |
274 | while(!CheckDelay(timer)); |
Line 240... | Line 275... | ||
240 | 275 | ||
241 | // If thrust is less than 100, stop calibration with a delay of 0.5 seconds |
276 | // If thrust is less than 100, stop calibration with a delay of 0.5 seconds |
242 | if (PPM_in[ParamSet.ChannelAssignment[CH_THRUST]] < 100) measurement--; |
277 | if (PPM_in[ParamSet.ChannelAssignment[CH_THRUST]] < 100) measurement--; |
- | 278 | } |
|
243 | } |
279 | if(!MM3_Timeout) |
244 | 280 | { |
|
245 | // Rage of all axis |
281 | // Rage of all axis |
246 | MM3_calib.X_range = (x_max - x_min); |
282 | MM3_calib.X_range = (x_max - x_min); |
247 | MM3_calib.Y_range = (y_max - y_min); |
283 | MM3_calib.Y_range = (y_max - y_min); |
248 | MM3_calib.Z_range = (z_max - z_min); |
284 | MM3_calib.Z_range = (z_max - z_min); |
249 | 285 | ||
250 | // Offset of all axis |
286 | // Offset of all axis |
251 | MM3_calib.X_off = (x_max + x_min) / 2; |
287 | MM3_calib.X_off = (x_max + x_min) / 2; |
252 | MM3_calib.Y_off = (y_max + y_min) / 2; |
288 | MM3_calib.Y_off = (y_max + y_min) / 2; |
253 | MM3_calib.Z_off = (z_max + z_min) / 2; |
289 | MM3_calib.Z_off = (z_max + z_min) / 2; |
254 | 290 | ||
255 | // save to EEProm |
291 | // save to EEProm |
256 | SetParamByte(PID_MM3_X_OFF, (uint8_t)MM3_calib.X_off); |
292 | SetParamByte(PID_MM3_X_OFF, (uint8_t)MM3_calib.X_off); |
257 | SetParamByte(PID_MM3_Y_OFF, (uint8_t)MM3_calib.Y_off); |
293 | SetParamByte(PID_MM3_Y_OFF, (uint8_t)MM3_calib.Y_off); |
258 | SetParamByte(PID_MM3_Z_OFF, (uint8_t)MM3_calib.Z_off); |
294 | SetParamByte(PID_MM3_Z_OFF, (uint8_t)MM3_calib.Z_off); |
259 | SetParamWord(PID_MM3_X_RANGE, (uint16_t)MM3_calib.X_range); |
295 | SetParamWord(PID_MM3_X_RANGE, (uint16_t)MM3_calib.X_range); |
260 | SetParamWord(PID_MM3_Y_RANGE, (uint16_t)MM3_calib.Y_range); |
296 | SetParamWord(PID_MM3_Y_RANGE, (uint16_t)MM3_calib.Y_range); |
- | 297 | SetParamWord(PID_MM3_Z_RANGE, (uint16_t)MM3_calib.Z_range); |
|
261 | SetParamWord(PID_MM3_Z_RANGE, (uint16_t)MM3_calib.Z_range); |
298 | } |
Line 262... | Line 299... | ||
262 | } |
299 | } |
263 | 300 | ||
Line 271... | Line 308... | ||
271 | int32_t Hx, Hy, Hz, Hx_corr, Hy_corr; |
308 | int32_t Hx, Hy, Hz, Hx_corr, Hy_corr; |
272 | int16_t angle; |
309 | int16_t angle; |
273 | uint16_t div_factor; |
310 | uint16_t div_factor; |
274 | int16_t heading; |
311 | int16_t heading; |
Line 275... | Line -... | ||
275 | - | ||
276 | // calibration factor for transforming Gyro Integrals to angular degrees |
- | |
277 | div_factor = (uint16_t)ParamSet.UserParam3 * 8; |
- | |
278 | - | ||
279 | // Offset correction and normalization (values of H are +/- 512) |
- | |
280 | Hx = (((int32_t)(MM3.x_axis - MM3_calib.X_off)) * 1024) / (int32_t)MM3_calib.X_range; |
- | |
281 | Hy = (((int32_t)(MM3.y_axis - MM3_calib.Y_off)) * 1024) / (int32_t)MM3_calib.Y_range; |
- | |
282 | Hz = (((int32_t)(MM3.z_axis - MM3_calib.Z_off)) * 1024) / (int32_t)MM3_calib.Z_range; |
- | |
283 | - | ||
284 | // Compensate the angle of the MM3-arrow to the head of the MK by a yaw rotation transformation |
- | |
285 | // assuming the MM3 board is mounted parallel to the frame. |
- | |
286 | // User Param 4 is used to define the positive angle from the MM3-arrow to the MK heading |
- | |
287 | // in a top view counter clockwise direction. |
- | |
288 | // North is in opposite direction of the small arrow on the MM3 board. |
- | |
289 | // Therefore 180 deg must be added to that angle. |
- | |
290 | angle = ((int16_t)ParamSet.UserParam4 + 180); |
- | |
291 | // wrap angle to interval of 0°- 359° |
- | |
292 | angle += 360; |
- | |
293 | angle %= 360; |
- | |
294 | sin_yaw = (int32_t)(c_sin_8192(angle)); |
- | |
295 | cos_yaw = (int32_t)(c_cos_8192(angle)); |
- | |
296 | - | ||
297 | Hx_corr = Hx; |
- | |
298 | Hy_corr = Hy; |
- | |
299 | - | ||
300 | // rotate |
- | |
301 | Hx = (Hx_corr * cos_yaw - Hy_corr * sin_yaw) / 8192; |
- | |
302 | Hy = (Hx_corr * sin_yaw + Hy_corr * cos_yaw) / 8192; |
- | |
303 | - | ||
304 | 312 | ||
305 | // tilt compensation |
313 | if (MM3_Timeout) |
306 | 314 | { |
|
307 | // calibration factor for transforming Gyro Integrals to angular degrees |
315 | // calibration factor for transforming Gyro Integrals to angular degrees |
308 | div_factor = (uint16_t)ParamSet.UserParam3 * 8; |
- | |
309 | - | ||
310 | // calculate sinus cosinus of pitch and tilt angle |
- | |
311 | angle = (IntegralPitch/div_factor); |
- | |
312 | sin_pitch = (int32_t)(c_sin_8192(angle)); |
- | |
313 | cos_pitch = (int32_t)(c_cos_8192(angle)); |
- | |
314 | - | ||
315 | angle = (IntegralRoll/div_factor); |
- | |
316 | sin_roll = (int32_t)(c_sin_8192(angle)); |
- | |
317 | cos_roll = (int32_t)(c_cos_8192(angle)); |
- | |
318 | - | ||
319 | Hx_corr = Hx * cos_pitch; |
- | |
320 | Hx_corr -= Hz * sin_pitch; |
- | |
321 | Hx_corr /= 8192; |
- | |
322 | - | ||
323 | Hy_corr = Hy * cos_roll; |
- | |
324 | Hy_corr += Hz * sin_roll; |
- | |
325 | Hy_corr /= 8192; |
- | |
326 | - | ||
327 | // calculate Heading |
- | |
328 | heading = c_atan2(Hy_corr, Hx_corr); |
- | |
329 | - | ||
330 | // atan returns angular range from -180 deg to 180 deg in counter clockwise notation |
- | |
331 | // but the compass course is defined in a range from 0 deg to 360 deg clockwise notation. |
- | |
332 | if (heading < 0) heading = -heading; |
- | |
Line -... | Line 316... | ||
- | 316 | div_factor = (uint16_t)ParamSet.UserParam3 * 8; |
|
- | 317 | ||
- | 318 | // Offset correction and normalization (values of H are +/- 512) |
|
- | 319 | Hx = (((int32_t)(MM3.x_axis - MM3_calib.X_off)) * 1024) / (int32_t)MM3_calib.X_range; |
|
- | 320 | Hy = (((int32_t)(MM3.y_axis - MM3_calib.Y_off)) * 1024) / (int32_t)MM3_calib.Y_range; |
|
- | 321 | Hz = (((int32_t)(MM3.z_axis - MM3_calib.Z_off)) * 1024) / (int32_t)MM3_calib.Z_range; |
|
- | 322 | ||
- | 323 | // Compensate the angle of the MM3-arrow to the head of the MK by a yaw rotation transformation |
|
- | 324 | // assuming the MM3 board is mounted parallel to the frame. |
|
- | 325 | // User Param 4 is used to define the positive angle from the MM3-arrow to the MK heading |
|
- | 326 | // in a top view counter clockwise direction. |
|
- | 327 | // North is in opposite direction of the small arrow on the MM3 board. |
|
- | 328 | // Therefore 180 deg must be added to that angle. |
|
- | 329 | angle = ((int16_t)ParamSet.UserParam4 + 180); |
|
- | 330 | // wrap angle to interval of 0°- 359° |
|
- | 331 | angle += 360; |
|
- | 332 | angle %= 360; |
|
- | 333 | sin_yaw = (int32_t)(c_sin_8192(angle)); |
|
- | 334 | cos_yaw = (int32_t)(c_cos_8192(angle)); |
|
- | 335 | ||
- | 336 | Hx_corr = Hx; |
|
- | 337 | Hy_corr = Hy; |
|
- | 338 | ||
- | 339 | // rotate |
|
- | 340 | Hx = (Hx_corr * cos_yaw - Hy_corr * sin_yaw) / 8192; |
|
- | 341 | Hy = (Hx_corr * sin_yaw + Hy_corr * cos_yaw) / 8192; |
|
- | 342 | ||
- | 343 | ||
- | 344 | // tilt compensation |
|
- | 345 | ||
- | 346 | // calibration factor for transforming Gyro Integrals to angular degrees |
|
- | 347 | div_factor = (uint16_t)ParamSet.UserParam3 * 8; |
|
- | 348 | ||
- | 349 | // calculate sinus cosinus of pitch and tilt angle |
|
- | 350 | angle = (IntegralPitch/div_factor); |
|
- | 351 | sin_pitch = (int32_t)(c_sin_8192(angle)); |
|
- | 352 | cos_pitch = (int32_t)(c_cos_8192(angle)); |
|
- | 353 | ||
- | 354 | angle = (IntegralRoll/div_factor); |
|
- | 355 | sin_roll = (int32_t)(c_sin_8192(angle)); |
|
- | 356 | cos_roll = (int32_t)(c_cos_8192(angle)); |
|
- | 357 | ||
- | 358 | Hx_corr = Hx * cos_pitch; |
|
- | 359 | Hx_corr -= Hz * sin_pitch; |
|
- | 360 | Hx_corr /= 8192; |
|
- | 361 | ||
- | 362 | Hy_corr = Hy * cos_roll; |
|
- | 363 | Hy_corr += Hz * sin_roll; |
|
- | 364 | Hy_corr /= 8192; |
|
- | 365 | ||
- | 366 | // calculate Heading |
|
- | 367 | heading = c_atan2(Hy_corr, Hx_corr); |
|
- | 368 | ||
- | 369 | // atan returns angular range from -180 deg to 180 deg in counter clockwise notation |
|
- | 370 | // but the compass course is defined in a range from 0 deg to 360 deg clockwise notation. |
|
- | 371 | if (heading < 0) heading = -heading; |
|
- | 372 | else heading = 360 - heading; |
|
- | 373 | } |
|
- | 374 | else // MM3_Timeout = 0 i.e now new data from external board |
|
- | 375 | { |
|
333 | else heading = 360 - heading; |
376 | heading = -1; |
334 | 377 | } |