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148 Commits

Author SHA1 Message Date
rmackay9 4877348c49 ArduCopter: remove some unhelpful constraints on nav_lat and nav_lon. 
Increase other constraints from 3200 to 32000.  These constraints are there to ensure int32_t do not cause an overflow when added to an int16_t.
 2012-10-24 22:04:35 +09:00
rmackay9 5e8043fd9c ArduCopter: changed ACRO_ROLL_STABILIZE and ACRO_PITCH_STABILIZE to parameters 
Changes on behalf of Leonard Hall
 2012-10-23 21:30:50 +09:00
Jason Short a0752dc7dc ACM Acceleration management 
removed unused waypoint_radius var
removed slow_wp
updated speed management system to maintain a constant acceleration or deceleration of 1m/s
changed version to 2.8.1a
 2012-10-21 14:32:39 -07:00
rmackay9 583f2e49a3 ArduCopter: integrated Leonard Hall's improved ACRO mode 2012-10-18 23:24:34 +09:00
rmackay9 b944d9df26 ArduCopter: bug fix in earthframe->body frame translation. 
Provided by Leonard Hall.

Also removed large unnecessary comments.
 2012-10-17 19:15:25 +09:00
rmackay9 5fbe53a84d ArduCopter: bug fix for get_yaw_rate_stabilized_ef 
Provided by Leonard Hall
 2012-10-17 10:18:24 +09:00
LeonardTHall d7b7e1cefa New Yaw controller using rate feed forward and stabilize. 
Signed-off-by: LeonardTHall <LeonardTHall@gmail.com>
 2012-10-15 11:37:49 +09:00
rmackay9 997fe85880 ArduCopter: fixed acro mode 
Changes included:
Removing earth frame roll_rate_trim, pitch_rate_trim and yaw_rate_trim.
Switch ACRO mode to use YAW_ACRO instead of YAW_HOLD.
Changed YAW_ACRO to use stabilize yaw when axis_enabled.
Reset ACRO roll, pitch and yaw targets to current attitude when first entering ACRO.
 2012-10-14 17:47:46 +09:00
rmackay9 2848bb8ee6 ArduCopter: freeze I terms if motor limits breached 2012-10-11 17:20:00 +09:00
rmackay9 7cf60e61b4 ArduCopter: bug fix in earth-frame to body-frame conversion for roll 2012-10-07 19:14:40 +09:00
rmackay9 05fd04134a ArduCopter: fix heli build 2012-10-06 13:46:19 +09:00
rmackay9 e375a27058 ArduCopter: prioritise rate controllers, rate controller targets converted to body frame 2012-10-03 14:10:31 +09:00
rmackay9 361ff0c08f ArduCopter: allow PID logging of throttle. Make get_angle_boost actually use parameter passed in. 2012-09-18 23:19:23 +09:00
uncrustify f783ace0de uncrustify ArduCopter/Attitude.pde 2012-08-21 19:19:50 -07:00
Jason Short 0a25a189eb ACM | Attitude.pde - removed next_wp.alt reset. 2012-08-18 12:25:48 -07:00
Jason Short bc631b656e ACM: Added a more sane limit to Angle boost 2012-08-18 09:04:21 -07:00
rmackay9 87d5b5944d ArduCopter: commented out get_acro_yaw2 function to reduce compiler warnings 2012-08-18 16:03:49 +09:00
rmackay9 92688a793a ArduCopter: fixed compiler warning related to shadowing of control_roll and control_pitch in get_of_roll and get_of_pitch. 2012-08-18 11:48:12 +09:00
Jason Short 9cee1b2fa0 ACM : Upped Yaw Limit to 2200 2012-08-16 15:38:46 -07:00
rmackay9 36f947acb9 ArduCopter: changed all "int" to "int16_t" and a few "long"s to "int32_t". 
Also moved "simple_counter" variable from global scope to the "update_simple_mode" function which is the only place that it's actually used.
 2012-08-16 20:04:46 +09:00
rmackay9 a72bf6ef57 ArduCopter: replaced abs with labs as required in a few places. 
Also fixed a small bug in the get_stabilize_pitch function in which it was using the roll (instead of pitch) to decide whether it should let the i term build-up or not.
 2012-08-16 17:51:09 +09:00
Jason Short 3ad08b7ffc ACM : Added larger WP radius for fast waypoints so we don't loose speed angling in on the WP at the last second. 2012-08-10 10:02:32 -07:00
Jason Short 132ac7d412 ACM : attitude.pde - removed unused function 2012-08-09 17:04:12 -07:00
Jason Short 5d756decd2 ACM : Attitude.pde 
yaw limit, moved toy code out of att to it's own pre
 2012-08-09 16:59:43 -07:00
Jason Short 8c47b0c087 ACM: Toy mode fix - Pitch flipped the sign on roll/Yaw coupling. 2012-07-30 15:43:05 -07:00
Jason Short 613849a8df Arducopter: Force nav_yaw to match auto_yaw when starting a mission 2012-07-19 22:59:03 -07:00
Jason Short 610d1d1795 Arducopter: deprecated the get_nav_yaw_offset function. 
Small Toy mode updates
 2012-07-19 17:41:52 -07:00
Jason Short aa645afe2b Arducopter: Altitude change nav 
Split altitude hold into two controls to parallel navigation.
 2012-07-18 22:57:10 -07:00
Jason Short 584e7dcda4 Arducopter: Removed Yaw Limit for Quads 2012-07-14 14:06:34 -07:00
Jason Short 44b16b7b61 Arducopter: Temp reversion to old Yaw controller. 2012-07-14 12:26:13 -07:00
Robert Lefebvre 59e133235f Implementing Yaw Fix. Tried to blend with Jason's changes. 2012-07-14 00:24:22 -04:00
Jason Short 6f9e2bf3a8 Arducopter: Toy mode update 
Removed debugging printfs,
lowered roll response - was too high in test flights
made roll limit 2500 for testing
 2012-07-11 17:46:06 -07:00
Jason Short 1feaaa4655 Arducopter: Toy mode refinements 2012-07-10 21:53:38 -07:00
Jason Short 226bba48a6 Toy Mode Yaw Rate fix 2012-07-09 13:13:32 -07:00
Jason Short c62706ad06 Toy Mode: Yaw performance update. 2012-07-03 17:14:54 -07:00
Jason Short 16b25a26c2 Toy Mode: removed virtual WP, copter now just goes into auto_loiter when not holding the sticks. 2012-07-02 17:52:38 -07:00
Jason Short e0b3309500 Yaw mode: 
Improved hybrid Yaw mode:
- uses rate controller rather than as fast as possible
- waits 1.5 seconds before entering hold
- bounce free
 2012-07-01 13:40:12 -07:00
Jason Short 3ce867508b Attitude.pde: Toy mode logic 2012-06-29 21:20:27 -07:00
Jason Short eeab4c5363 Attitude.pde: Turned off boost_p for nav_throttle based on Testing feedback from Marco. 2012-06-26 10:39:42 -07:00
Jason Short 812bf7d874 Attitude.pde - Added small boost to alt hold for takeoff. 2012-06-25 23:12:19 -07:00
Robert Lefebvre 1064dcbd34 Open up constraint on Rate Yaw Output for all copters. 2012-06-22 10:06:01 -04:00
Jason Short 27e0aee03f Small fix to angle boost - increases by about 20% to deal with inefficiencies of non-downward thrust 2012-06-20 08:47:47 -07:00
Jason Short c42f9ece43 Inertial Control 
I added inertial navigation based on the simulator data. This is an option only available if you compile with Arduino and set
#define INERTIAL_NAV ENABLED
in the APM_Config.h file.

This has been tested for one real flight and did not crash my quad, but consider it very alpha. The quad may be unpredictable at first until the error correction fixes poorly calibrated accels. Be Careful.

Most of the real work is in the inertia file, but the error correction, new variable defines and calibration calls are sprinkled throughout.

The Log should record RAW messages with special debugging values.
 2012-06-13 22:34:45 -07:00
rmackay9 65050775e1 ArduCopter: made Robert's new yaw method optional (off by default). 
Add this line to APM_Config.h to enable Robert's yaw
#define ALTERNATIVE_YAW_MODE ENABLED
 2012-06-13 21:50:16 +09:00
Robert Lefebvre c5916a8b4d Opening up the Yaw Rate constraint for Trad Heli. 2012-06-07 22:40:25 -04:00
Robert Lefebvre e2496181ff Yaw Fix 
Modified Nav_Yaw controller to better track intended heading changes.
 2012-06-07 17:15:33 -04:00
Jason Short a9610a0761 Stabilization patches 
removed Angle error limit for stabilization
constricted Iterm to +- 5° error and limited the implementation to when the quad is +- 5° from center
doubled the output limit for Rate controller.
increased default Rate_P gain to .18 with matching Rate_D of .004
Tested in the SIM and in backyard. dramatically increases performance and quad no longer overshoots and flips when pushed hard.
 2012-06-05 16:41:44 -07:00
Jason Short 9ab06c5542 Moved PID logging counter into define 2012-06-03 11:13:50 -07:00
Jason Short 2311d52d37 Renamed some variables to clarify functionality. 2012-05-29 12:42:37 -07:00
Jason Short 1a5e2f4e37 Attitude.pde - Removed rate limit based on SIM flights. These should never have been in place and seriously detriment Acro flight. 2012-05-21 09:58:23 -07:00