Paparazzi UAS  v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
optical_flow_hover.c
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1 /*
2  * Copyright (C) 2018
3  *
4  * This file is part of paparazzi.
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14  * GNU General Public License for more details.
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18  * <http://www.gnu.org/licenses/>.
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20 
21 #include "optical_flow_hover.h"
22 #include "optical_flow_functions.h"
23 
24 #include "generated/airframe.h"
25 #include "autopilot.h"
26 #include "paparazzi.h"
27 #include "modules/core/abi.h"
32 #include <stdio.h>
33 
35 //
37 #include "mcu_periph/sys_time.h"
38 //
39 // Additional math functions
40 #include "math/pprz_stat.h"
41 
42 /* Use optical flow estimates */
43 #ifndef OFH_OPTICAL_FLOW_ID
44 #define OFH_OPTICAL_FLOW_ID ABI_BROADCAST
45 #endif
47 
48 // Set the standard method (1) to apply the algorithm to all 3 axes at the same time
49 #ifndef OFH_HOVER_METHOD
50 #define OFH_HOVER_METHOD 1
51 #endif
52 
53 // Set the standard method to assume the quadrotor is not (0) symmetrical
54 #ifndef XY_SYMMETRICAL
55 #define XY_SYMMETRICAL 0
56 #endif
57 
58 // Set the standard method to use vision signal and the known input and signal (0) optionally one can use the autocovariance (1)
59 #ifndef OFH_COV_METHOD
60 #define OFH_COV_METHOD 0
61 #endif
62 
63 // number of time steps used for calculating the covariance (oscillations) and the delay steps
64 #ifndef COV_WINDOW_SIZE
65 #define COV_WINDOW_SIZE (10*30)
66 #endif
67 
68 // In case the autocovariance is used, select half the window size as the delay
69 #ifndef OF_COV_DELAY_STEPS
70 #define OF_COV_DELAY_STEPS COV_WINDOW_SIZE/2
71 #endif
72 
73 // The low pass filter constant for updating the vision measurements in the algorithm
74 #ifndef OF_LP_CONST
75 #define OF_LP_CONST 0.5
76 #endif
77 
78 // Whether the algorithm should be applied to the phi angle(1) or not(0)
79 #ifndef OFH_OSCPHI
80 #define OFH_OSCPHI 1
81 #endif
82 
83 // Whether the algorithm should be applied to the theta angle(1) or not(0)
84 #ifndef OFH_OSCTHETA
85 #define OFH_OSCTHETA 1
86 #endif
87 
88 // Use default PID gains
89 #ifndef OFH_PGAINZ
90 #define OFH_PGAINZ 0.4
91 #endif
92 
93 #ifndef OFH_IGAINZ
94 #define OFH_IGAINZ 0.f
95 #endif
96 
97 #ifndef OFH_DGAINZ
98 #define OFH_DGAINZ 0.0
99 #endif
100 
101 // Default slope at which the gain is increased
102 #ifndef OFH_RAMPZ
103 #define OFH_RAMPZ 0.15
104 #endif
105 
106 // Default reduction factor to stabilize the quad after oscillating
107 #ifndef OFH_REDUCTIONZ
108 #define OFH_REDUCTIONZ 0.45
109 #endif
110 
111 // The threshold value for the covariance oscillation measurement
112 #ifndef OFH_COVDIV_SETPOINT
113 #define OFH_COVDIV_SETPOINT -0.02
114 #endif
115 
116 // Use default PID gains
117 #ifndef OFH_PGAINX
118 #define OFH_PGAINX 0.f
119 #endif
120 
121 #ifndef OFH_IGAINX
122 #define OFH_IGAINX 0.00002
123 #endif
124 
125 #ifndef OFH_DGAINX
126 #define OFH_DGAINX 0.f
127 #endif
128 
129 #ifndef OFH_PGAINY
130 #define OFH_PGAINY 0.f
131 #endif
132 
133 #ifndef OFH_IGAINY
134 #define OFH_IGAINY 0.00002
135 #endif
136 
137 #ifndef OFH_DGAINY
138 #define OFH_DGAINY 0.f
139 #endif
140 
141 // Default slope at which the gain is increased
142 #ifndef OFH_RAMPXY
143 #define OFH_RAMPXY 0.0008
144 #endif
145 
146 // Default reduction factor to stabilize the quad after oscillating
147 #ifndef OFH_REDUCTIONXY
148 #define OFH_REDUCTIONXY 0.3
149 #endif
150 
151 // The threshold value for the covariance oscillation measurement
152 #ifndef OFH_COVFLOW_SETPOINT
153 #define OFH_COVFLOW_SETPOINT -500.f
154 #endif
155 
156 // The default slopes for the height-gain relationships
157 #ifndef OFH_VER_SLOPE_A
158 #define OFH_VER_SLOPE_A 0.5
159 #endif
160 
161 #ifndef OFH_VER_SLOPE_B
162 #define OFH_VER_SLOPE_B 0.25
163 #endif
164 
165 #ifndef OFH_HOR_X_SLOPE_A
166 #define OFH_HOR_X_SLOPE_A 2.f
167 #endif
168 
169 #ifndef OFH_HOR_X_SLOPE_B
170 #define OFH_HOR_X_SLOPE_B 0.5
171 #endif
172 
173 #ifndef OFH_HOR_Y_SLOPE_A
174 #define OFH_HOR_Y_SLOPE_A OFH_HOR_X_SLOPE_A
175 #endif
176 
177 #ifndef OFH_HOR_Y_SLOPE_B
178 #define OFH_HOR_Y_SLOPE_B OFH_HOR_X_SLOPE_B
179 #endif
180 
181 
183 struct FloatVect3 covariances;
184 
185 // variables retained between module calls
187 
192 struct OFhistory historyX;
193 struct OFhistory historyY;
194 
195 // Stabilizing commands
196 struct Int32Eulers ofh_sp_eu;
197 
200 
201 struct OFhistory historyZ;
202 
203 // The optical flow ABI event
205 
206 // struct containing most relevant parameters
210 
211 // variables used in the GCS
212 bool oscphi;
213 bool osctheta;
217 
218 
220 // Callback function of the optical flow estimate:
221 void ofh_optical_flow_cb(uint8_t sender_id __attribute__((unused)), uint32_t stamp, int32_t flow_x, int32_t flow_y,
222  int32_t flow_der_x, int32_t flow_der_y, float quality, float size_div);
223 
224 // resetting all variables to be called for instance when starting up / re-entering module
225 static void reset_horizontal_vars(void);
226 static void reset_vertical_vars(void);
227 void vertical_ctrl_module_run(void);
228 void horizontal_ctrl_module_run(void);
229 
230 // Compute OptiTrack stabilization for 1/2 axes
231 void computeOptiTrack(bool phi, bool theta, struct Int32Eulers *opti_sp_eu);
232 #ifndef GH_GAIN_SCALE
233 #define GH_GAIN_SCALE 2
234 #endif
235 #ifndef MAX_POS_ERR
236 #define MAX_POS_ERR POS_BFP_OF_REAL(16.)
237 #endif
238 #ifndef MAX_SPEED_ERR
239 #define MAX_SPEED_ERR SPEED_BFP_OF_REAL(16.)
240 #endif
246 
247 
248 // sending the divergence message to the ground station:
249 static void send_optical_flow_hover(struct transport_tx *trans, struct link_device *dev)
250 {
251  pprz_msg_send_OPTICAL_FLOW_HOVER(trans, dev, AC_ID, &of_hover.flowX, &of_hover.flowY, &of_hover.divergence,
255 }
256 
257 
258 // Init the optical flow hover module
260 {
261  of_hover_ctrl_X.setpoint = 0.0f;
268 
269  of_hover_ctrl_Y.setpoint = 0.0f;
276 
277  of_hover_ctrl_Z.setpoint = 0.0f;
284 
285  oscphi = OFH_OSCPHI;
287 
290 
293 
294  // Subscribe to the optical flow estimator:
295  AbiBindMsgOPTICAL_FLOW(OFH_OPTICAL_FLOW_ID, &optical_flow_ev, ofh_optical_flow_cb);
296 
297  // register telemetry:
298  register_periodic_telemetry(DefaultPeriodic, PPRZ_MSG_ID_OPTICAL_FLOW_HOVER, send_optical_flow_hover);
299 }
300 
304 static void reset_horizontal_vars(void)
305 {
306  // Take the current angles as neutral
307  struct Int32Eulers tempangle = stab_sp_to_eulers_i(&stabilization.sp);
310 
311  des_inputs.phi = 0;
312  des_inputs.theta = 0;
313 
314  // FIXME module is always used for vertical control
315  if ((hover_method == 0)) {
316  // Z - X - Y Order
317  oscillatingX = 1;
318  oscillatingY = 1;
321  } else if ((hover_method == 2)) {
322  // Z Set XY
323  oscillatingX = 1;
324  oscillatingY = 1;
327  of_hover_ctrl_X.PID.I = OFH_IGAINX / 4; // Have a slighly lower I gain during Z
328  of_hover_ctrl_Y.PID.I = OFH_IGAINY / 4; // Have a slighly lower I gain during Z
329  } else {
330  // if V is in NAV or hover_method = 1 FIXME NAV is not called for vertical
331  //All axes
332  oscillatingX = 0;
333  oscillatingY = 0;
336  }
337 
338  flowX = 0;
339  flowY = 0;
340 
341  of_hover_ctrl_X.PID.sum_err = 0.0f;
342  of_hover_ctrl_X.PID.d_err = 0.0f;
344 
345  of_hover_ctrl_Y.PID.sum_err = 0.0f;
346  of_hover_ctrl_Y.PID.d_err = 0.0f;
348 
351 
352  ind_histXY = 0;
353  cov_array_filledXY = 0;
354 
355  covariances.x = 0.0f;
356  covariances.y = 0.0f;
357 
358  for (uint16_t i = 0; i < COV_WINDOW_SIZE; i++) {
359  historyX.OF[i] = 0.0f;
360  historyY.OF[i] = 0.0f;
361  historyX.past_OF[i] = 0.0f;
362  historyY.past_OF[i] = 0.0f;
363  historyX.input[i] = 0.0f;
364  historyY.input[i] = 0.0f;
365  }
366 
367  of_hover.flowX = 0;
368  of_hover.flowY = 0;
369 
372 }
373 
377 static void reset_vertical_vars(void)
378 {
379  oscillatingZ = 0;
380 
381  divergence_vision = 0;
382  of_hover.divergence = 0;
383 
384  for (uint16_t i = 0; i < COV_WINDOW_SIZE; i++) {
385  historyZ.OF[i] = 0.0f;
386  historyZ.past_OF[i] = 0.0f;
387  historyZ.input[i] = 0.0f;
388  }
389 
390  ind_histZ = 0;
391 
392  covariances.z = 0.0f;
393  cov_array_filledZ = 0;
394 
396 
397  of_hover_ctrl_Z.PID.sum_err = 0.0f;
398  of_hover_ctrl_Z.PID.d_err = 0.0f;
400 
403 }
404 
405 
410 {
411  /***********
412  * TIME
413  ***********/
414  float ventral_factor = -1.28f; // magic number comprising field of view etc.
415 
416  float dt = vision_time - prev_vision_timeXY;
417 
418  // check if new measurement received
419  if (dt <= 1e-5f) {
420  return;
421  }
422 
423  /***********
424  * VISION
425  ***********/
426 
427  float lp_factor = dt / OF_LP_CONST;
428  Bound(lp_factor, 0.f, 1.f);
429 
430  float new_flowX = (flowX * ventral_factor) / dt;
431  float new_flowY = (flowY * ventral_factor) / dt;
432 
433  //TODO: deal with (unlikely) fast changes in Flow?
434 
435  // low-pass filter the divergence:
436  of_hover.flowX += (new_flowX - of_hover.flowX) * lp_factor;
437  of_hover.flowY += (new_flowY - of_hover.flowY) * lp_factor;
438 
439 
440  /***********
441  * CONTROL
442  ***********/
443 
444  if (!oscillatingX) {
445  // if not oscillating, increase gain
447  }
448  if (!oscillatingY) {
449  // if not oscillating, increase gain
451  }
452 
453  // set desired pitch en roll
454  if (oscphi) {
457  }
458  if (osctheta) {
461  }
462 
463  // update covariance
467 
468  // Check for oscillations
470  oscillatingX = 1;
471 
472  if (hover_method == 0) {
473  //Start the Y axis
474  oscillatingY = 0;
476  }
478 
479  if (XY_SYMMETRICAL) {
480  // also set Y
481  oscillatingY = 1;
483  }
484  }
486  oscillatingY = 1;
488  }
489 
490  // Compute 0, 1 or 2 horizontal axes with optitrack
492 
494 }
495 
500 {
501  /***********
502  * TIME
503  ***********/
504 
505  float div_factor; // factor that maps divergence in pixels as received from vision to 1 / frame
506 
507  float dt = vision_time - prev_vision_timeZ;
508 
509  // check if new measurement received
510  if (dt <= 1e-5f) {
511  return;
512  }
513 
514  /***********
515  * VISION
516  ***********/
517 
518  float lp_factor = dt / OF_LP_CONST;
519  Bound(lp_factor, 0.f, 1.f);
520 
521  // Vision
522  div_factor = -1.28f; // magic number comprising field of view etc.
523  float new_divergence = (divergence_vision * div_factor) / dt;
524 
525  // deal with (unlikely) fast changes in divergence:
526  static const float max_div_dt = 0.20f;
527  if (fabsf(new_divergence - of_hover.divergence) > max_div_dt) {
528  if (new_divergence < of_hover.divergence) { new_divergence = of_hover.divergence - max_div_dt; }
529  else { new_divergence = of_hover.divergence + max_div_dt; }
530  }
531  // low-pass filter the divergence:
532 
533  of_hover.divergence += (new_divergence - of_hover.divergence) * lp_factor;
535 
536  /***********
537  * CONTROL
538  ***********/
539  if (!oscillatingZ) {
540  // if not oscillating, increase gain
542  }
543 
544  // use the divergence for control:
547 
549 
550  // Check for oscillations
552  float estimatedHeight = of_hover_ctrl_Z.PID.P * OFH_VER_SLOPE_A + OFH_VER_SLOPE_B; // Vertical slope Z
553  oscillatingZ = 1;
554  of_hover_ctrl_Z.setpoint = 0.0f;
556 
557  if (hover_method == 0) {
558  // Z- X - Y Order
559  // Start the X axis
560  oscillatingX = 0;
562  } else if (hover_method == 2) {
563  // Start XY axes with computed slope
564  of_hover_ctrl_X.PID.sum_err = 0.0f;
565  of_hover_ctrl_Y.PID.sum_err = 0.0f;
568  of_hover_ctrl_X.PID.P = OFH_REDUCTIONXY * (estimatedHeight * OFH_HOR_X_SLOPE_A - OFH_HOR_X_SLOPE_B); // Horizontal Slope X
569  of_hover_ctrl_Y.PID.P = OFH_REDUCTIONXY * (estimatedHeight * OFH_HOR_Y_SLOPE_A - OFH_HOR_Y_SLOPE_B); // Horizontal Slope Y
570  } else {
571  // hover_method = 1
572  //All axes
573  }
574  }
575 
576 }
577 
578 void ofh_optical_flow_cb(uint8_t sender_id UNUSED, uint32_t stamp, int32_t flow_x, int32_t flow_y,
579  int32_t flow_der_x, int32_t flow_der_y, float quality UNUSED, float size_div)
580 {
581  if (!derotated) {
582  flowX = flow_x;
583  flowY = flow_y;
584  } else {
585  flowX = flow_der_x;
586  flowY = flow_der_y;
587  }
588 
589  divergence_vision = size_div;
590 
591  vision_time = ((float)stamp) / 1e6;
592 }
593 
595 // Call our controller
596 
601 {
603 
604  // adaptive estimation - assume hover condition when entering the module
605  of_hover_ctrl_Z.nominal_value = (float) stabilization.cmd[COMMAND_THRUST] / MAX_PPRZ;
607 
608  // Set current psi as heading
610 
613 }
614 
615 // Run the controller
616 void guidance_module_run(bool in_flight)
617 {
618  if (electrical.bat_low) {
620  } else {
621  // your controller goes here
626  stabilization_attitude_run(in_flight, &sp, &th, stabilization.cmd);
627  }
628 }
629 
636 void computeOptiTrack(bool phi, bool theta, struct Int32Eulers *opti_sp_eu)
637 {
638 
639  bool optiVelOnly;
640  optiVelOnly = 0;
641 
643 
644  struct NedCoor_i vel_from_GPS;
645  struct NedCoor_i pos_from_GPS;
646 
647  vel_from_GPS = *stateGetSpeedNed_i();
648  pos_from_GPS = *stateGetPositionNed_i();
649 
650  /* maximum bank angle: default 20 deg, max 40 deg*/
651  static const int32_t traj_max_bank = Min(BFP_OF_REAL(GUIDANCE_H_MAX_BANK, INT32_ANGLE_FRAC),
652  BFP_OF_REAL(RadOfDeg(40), INT32_ANGLE_FRAC));
653  static const int32_t total_max_bank = BFP_OF_REAL(RadOfDeg(45), INT32_ANGLE_FRAC);
654 
655  /* compute position error */
657  /* saturate it */
659 
660  struct Int32Vect2 ref_speed;
661  ref_speed.x = 0;
662  ref_speed.y = 0;
663 
664  /* compute speed error */
665  VECT2_DIFF(of_hover_speed_err, ref_speed, vel_from_GPS);
666  /* saturate it */
668 
669  if (optiVelOnly) {
670  of_hover_pos_err.x = 0;
671  of_hover_pos_err.y = 0;
672  }
673 
674  /* run PID */
676  ((GUIDANCE_H_PGAIN * of_hover_pos_err.x) >> (INT32_POS_FRAC - GH_GAIN_SCALE)) +
677  ((GUIDANCE_H_DGAIN * (of_hover_speed_err.x >> 2)) >> (INT32_SPEED_FRAC - GH_GAIN_SCALE - 2));
679  ((GUIDANCE_H_PGAIN * of_hover_pos_err.y) >> (INT32_POS_FRAC - GH_GAIN_SCALE)) +
680  ((GUIDANCE_H_DGAIN * (of_hover_speed_err.y >> 2)) >> (INT32_SPEED_FRAC - GH_GAIN_SCALE - 2));
681 
682  /* trim max bank angle from PD */
683  VECT2_STRIM(of_hover_cmd_earth, -traj_max_bank, traj_max_bank);
684 
685  of_hover_trim_att_integrator.x += (GUIDANCE_H_IGAIN * of_hover_cmd_earth.x);
686  of_hover_trim_att_integrator.y += (GUIDANCE_H_IGAIN * of_hover_cmd_earth.y);
687  /* saturate it */
689  (traj_max_bank << (INT32_ANGLE_FRAC + GH_GAIN_SCALE * 2)));
690 
691  /* add it to the command */
694 
695  VECT2_STRIM(of_hover_cmd_earth, -total_max_bank, total_max_bank);
696 
697  // Compute Angle Setpoints - Taken from Stab_att_quat
698  int32_t s_psi, c_psi;
699  PPRZ_ITRIG_SIN(s_psi, psi);
700  PPRZ_ITRIG_COS(c_psi, psi);
701 
702  if (phi) {
703  opti_sp_eu->phi = (-s_psi * of_hover_cmd_earth.x + c_psi * of_hover_cmd_earth.y) >> INT32_TRIG_FRAC;
704  }
705  if (theta) {
706  opti_sp_eu->theta = -(c_psi * of_hover_cmd_earth.x + s_psi * of_hover_cmd_earth.y) >> INT32_TRIG_FRAC;
707  }
708 }
709 
Main include for ABI (AirBorneInterface).
Event structure to store callbacks in a linked list.
Definition: abi_common.h:67
bool autopilot_set_mode(uint8_t new_autopilot_mode)
set autopilot mode
Definition: autopilot.c:193
Core autopilot interface common to all firmwares.
uint8_t last_wp UNUSED
struct Electrical electrical
Definition: electrical.c:92
Interface for electrical status: supply voltage, current, battery status, etc.
bool bat_low
battery low status
Definition: electrical.h:50
#define Min(x, y)
Definition: esc_dshot.c:109
#define VECT2_DIFF(_c, _a, _b)
Definition: pprz_algebra.h:92
#define VECT2_STRIM(_v, _min, _max)
Definition: pprz_algebra.h:110
#define VECT2_COPY(_a, _b)
Definition: pprz_algebra.h:68
int32_t phi
in rad with INT32_ANGLE_FRAC
int32_t psi
in rad with INT32_ANGLE_FRAC
int32_t theta
in rad with INT32_ANGLE_FRAC
#define INT32_POS_FRAC
#define INT32_TRIG_FRAC
#define INT32_SPEED_FRAC
#define FLOAT_OF_BFP(_vbfp, _frac)
#define INT32_ANGLE_FRAC
#define BFP_OF_REAL(_vr, _frac)
euler angles
vector in North East Down coordinates
static struct Int32Eulers * stateGetNedToBodyEulers_i(void)
Get vehicle body attitude euler angles (int).
Definition: state.h:1125
static struct NedCoor_i * stateGetPositionNed_i(void)
Get position in local NED coordinates (int).
Definition: state.h:665
static struct NedCoor_i * stateGetSpeedNed_i(void)
Get ground speed in local NED coordinates (int).
Definition: state.h:863
float lp_factor
Definition: ins_flow.c:187
PRINT_CONFIG_VAR(ONELOOP_ANDI_FILT_CUTOFF)
uint8_t cov_array_filledXY
int32_t PID_divergence_control(float dt, struct OpticalFlowHoverControl *of_hover_ctrl)
Determine and set the thrust for constant divergence control.
struct OpticalFlowHover of_hover
float set_cov_div(bool cov_method, struct OFhistory *history, struct DesiredInputs *inputs)
Set the covariance of the divergence and the thrust / past divergence This funciton should only be ca...
float PID_flow_control(float dt, struct OpticalFlowHoverControl *of_hover_ctrl)
Determine and set the desired angle for constant flow control.
uint32_t ind_histXY
uint32_t ind_histZ
uint8_t cov_array_filledZ
void set_cov_flow(bool cov_method, struct OFhistory *historyX, struct OFhistory *historyY, struct DesiredInputs *inputs, struct FloatVect3 *covs)
Set the covariance of the flow and past flow / desired angle This funciton should only be called once...
float cov_setpoint
for adaptive gain control, setpoint of the covariance (oscillations)
float d_err
difference of error for the D-gain
float P
P-gain for control.
float divergence
Divergence estimate.
struct GainsPID PID
The struct with the PID gains.
float flowX
Flow estimate in X direction.
float previous_err
Previous tracking error.
float I
I-gain for control.
float input[COV_WINDOW_SIZE]
float reduction_factor
Reduce the gain by this factor when oscillating.
float sum_err
integration of the error for I-gain
float past_OF[COV_WINDOW_SIZE]
float setpoint
setpoint for constant divergence/flow
float D
D-gain for control.
float flowY
Flow estimate in Y direction.
float nominal_value
The nominal value of thrust, phi or theta depending on Z, Y, X.
float OF[COV_WINDOW_SIZE]
float err
Current tracking error.
float ramp
The ramp pused is increased with per dt.
void ofh_optical_flow_cb(uint8_t sender_id, uint32_t stamp, int32_t flow_x, int32_t flow_y, int32_t flow_der_x, int32_t flow_der_y, float quality, float size_div)
Function definitions.
static void reset_horizontal_vars(void)
Reset all horizontal variables:
void computeOptiTrack(bool phi, bool theta, struct Int32Eulers *opti_sp_eu)
Get the desired Euler angles for optitrack stabilization.
static abi_event optical_flow_ev
static void send_optical_flow_hover(struct transport_tx *trans, struct link_device *dev)
float prev_vision_timeZ
void horizontal_ctrl_module_run(void)
Run the horizontal optical flow hover module.
bool oscillatingX
bool derotated
struct OpticalFlowHoverControl of_hover_ctrl_Y
#define OFH_REDUCTIONZ
#define MAX_SPEED_ERR
struct FloatVect3 covariances
struct Int32Vect2 of_hover_pos_err
int32_t flowX
struct Int32Vect2 of_hover_cmd_earth
#define OFH_DGAINZ
int32_t flowY
#define XY_SYMMETRICAL
struct DesiredInputs des_inputs
uint8_t hover_method
Method used to hover 0 = All axis after each other; 1 = all axis at the same time; 2 = vertical only,...
#define COV_WINDOW_SIZE
#define OFH_OSCTHETA
bool oscphi
#define OFH_IGAINY
#define OFH_IGAINZ
#define OFH_PGAINY
#define OFH_COV_METHOD
struct OpticalFlowHoverControl of_hover_ctrl_Z
#define OFH_HOR_X_SLOPE_B
#define OFH_HOR_X_SLOPE_A
struct OFhistory historyZ
float prev_vision_timeXY
#define MAX_POS_ERR
#define OFH_OPTICAL_FLOW_ID
float divergence_vision
#define OFH_HOVER_METHOD
#define OFH_PGAINX
void guidance_module_enter(void)
Entering the module (user switched to module)
void guidance_module_run(bool in_flight)
#define OFH_RAMPZ
struct OFhistory historyX
#define OFH_COVFLOW_SETPOINT
static void reset_vertical_vars(void)
Reset all vertical variables:
#define GH_GAIN_SCALE
bool oscillatingZ
#define OFH_REDUCTIONXY
void optical_flow_hover_init()
#define OFH_PGAINZ
#define OFH_DGAINX
#define OFH_VER_SLOPE_B
float vision_time
struct Int32Vect2 of_hover_ref_pos
#define OFH_DGAINY
struct OFhistory historyY
#define OFH_IGAINX
bool cov_method
method to calculate the covariance: between thrust and div / angle and flow (0) or div and div past /...
#define OFH_COVDIV_SETPOINT
struct Int32Vect2 of_hover_speed_err
struct OpticalFlowHoverControl of_hover_ctrl_X
#define OF_LP_CONST
struct Int32Eulers ofh_sp_eu
bool oscillatingY
void vertical_ctrl_module_run(void)
Run the vertical optical flow hover module.
#define OFH_RAMPXY
bool osctheta
#define OFH_VER_SLOPE_A
struct Int32Vect2 of_hover_trim_att_integrator
#define OFH_OSCPHI
#define OFH_HOR_Y_SLOPE_B
#define OFH_HOR_Y_SLOPE_A
#define MAX_PPRZ
Definition: paparazzi.h:8
Statistics functions.
#define PPRZ_ITRIG_SIN(_s, _a)
#define PPRZ_ITRIG_COS(_c, _a)
#define AP_MODE_NAV
#define GUIDANCE_H_MAX_BANK
Max bank controlled by guidance.
Definition: guidance_h.h:64
Vertical guidance for rotorcrafts.
General attitude stabilization interface for rotorcrafts.
void stabilization_attitude_run(bool in_flight, struct StabilizationSetpoint *sp, struct ThrustSetpoint *thrust, int32_t *cmd)
Attitude control run function.
struct Stabilization stabilization
Definition: stabilization.c:41
struct StabilizationSetpoint stab_sp_from_eulers_i(struct Int32Eulers *eulers)
struct Int32Eulers stab_sp_to_eulers_i(struct StabilizationSetpoint *sp)
struct ThrustSetpoint th_sp_from_thrust_i(int32_t thrust, uint8_t axis)
General stabilization interface for rotorcrafts.
struct StabilizationSetpoint sp
current attitude setpoint (store for messages)
#define THRUST_AXIS_Z
int32_t cmd[COMMANDS_NB]
output command vector, range from [-MAX_PPRZ:MAX_PPRZ] (store for messages)
static const struct usb_device_descriptor dev
Definition: usb_ser_hw.c:74
Stabilization setpoint.
Definition: stabilization.h:53
union StabilizationSetpoint::@278 sp
Thrust setpoint // TODO to a setpoint header Structure to store the desired thrust vector with differ...
Definition: stabilization.h:82
union ThrustSetpoint::@284 sp
Architecture independent timing functions.
static float get_sys_time_float(void)
Get the time in seconds since startup.
Definition: sys_time.h:138
int8_t register_periodic_telemetry(struct periodic_telemetry *_pt, uint8_t _id, telemetry_cb _cb)
Register a telemetry callback function.
Definition: telemetry.c:51
Periodic telemetry system header (includes downlink utility and generated code).
#define DefaultPeriodic
Set default periodic telemetry.
Definition: telemetry.h:66
unsigned short uint16_t
Typedef defining 16 bit unsigned short type.
Definition: vl53l1_types.h:88
int int32_t
Typedef defining 32 bit int type.
Definition: vl53l1_types.h:83
unsigned int uint32_t
Typedef defining 32 bit unsigned int type.
Definition: vl53l1_types.h:78
unsigned char uint8_t
Typedef defining 8 bit unsigned char type.
Definition: vl53l1_types.h:98