ardupilot

Commit Graph

Author	SHA1	Message	Date
rmackay9	a5bb54e36e	ArduCopter: RTL clean-up and slightly improved landing sensor Consolidated RTL state to be captured by rtl_state variable. Combined update_RTL_Nav and verify_RTL functions which performed the same function but one was for missions, the other for the RTL flight mode. Renamed some RTL parameters and global variables to have RTL at the front. Landing detector now checks accel-throttle's I term and/or a very low throttle value	12 years ago
rmackay9	072ffec493	ArduCopter: allow INERTIAL_NAV to be enabled separately for horizontal and vertical position	12 years ago
rmackay9	bdb47c449a	ArduCopter: pass linear altitude error to throttle rate controllers. Previously the requested rate used the square root of the altitude error. Scale pilot's desired vertical rate and acceleration based on ACCELERATION_MAX_Z and VELOCITY_MAX_Z #defines	12 years ago
rmackay9	7b4ed2d227	ArduCopter: restored landing detector to landing throttle mode. Added LAND_SPEED parameter to control the rate of descent for the last 10m of a landing. Added CH6 tuning for accel based throttle controller.	12 years ago
rmackay9	a94826f182	ArduCopter: add set_throttle_mode to better control initialisation of variables	12 years ago
rmackay9	1036b35128	ArduCopter: added back in angle boost and recombined for heli and multicopter	12 years ago
rmackay9	3cbef57c64	ArduCopter: first merge of leonard's accel based altitude controller plus other changes from Randy Changes include: New low-level get_throttle_accel function takes target acceleration and compares vs earth-frame Z accelerometer values to produce output to motors. Higher level throttle controllers modified to call new get_throttle_accel controller Throttle_rate_stabilized controller added which maintains a desired climb/descent rate Throttle_land controller added - descends using normal auto throttle controller to 10m then descends at 50cm/s Multiple throttle modes added including landing mode Land flight mode no longer needs GPS Throttle cruise maintenance moved to update_throttle_cruise function	12 years ago
Robert Lefebvre	1d589c0b7d	ACM: TradHeli Fixes for Attitude rate controllers.	12 years ago
Robert Lefebvre	07d7d90882	ACM: TradHeli Bringing in Low Pass Filter for Rate Controllers	12 years ago
Robert Lefebvre	3f0e8dd358	ACM: TradHeli Bringing in Low Pas Filter Commented out because it does not build. Needs updates to Low Pass Filter Lib	12 years ago
Robert Lefebvre	e8d619acad	ACM: Begin creation of TradHeli rate control. May affect Multi-Rotors.	12 years ago
Robert Lefebvre	95eeda7cf7	ACM: TradHeli Removing Angle Boost function. Does not make sense for helis due to aerodynamics. Can cause more problems than it solves.	12 years ago
Robert Lefebvre	6ffc115236	Changes to get_throttle_rate() Commented out a bit of code that is not used currently Change the output constrains to #defines so they can be easily changed, particularly for use in TradHeli.	12 years ago
rmackay9	07a7a1acd8	ArduCopter: replaced digitalRead and digitalWrite with faster calls improved performance logging to dataflash	12 years ago
Jason Short	5f57678a9c	ACM Nav_throttle- removed sign inversion	12 years ago
rmackay9	ac5dcc8d49	ArduCopter: remove last remanants of rate_d to resolve compiler warning of unused variables	12 years ago
Jason Short	69db678252	ACM: attitude.pde - adjusted the FF of the alt hold algorithm, the old way was pretty crap. increased the output range of rate controller.	12 years ago
Jason Short	5ad38a32bf	ACM : Attitude : added nav param reset	12 years ago
Jason Short	3c78c4a7a3	ACM : Attitude.pde added ap bitfield for failsafe bit	12 years ago
Jason Short	a42c6bb609	ACM : Attitude.pde removed stabilize D	12 years ago
rmackay9	14cbe37d3e	ArduCopter: remove unused get_stabilize_rate_yaw	12 years ago
rmackay9	1f801714e8	ArduCopter: incorporate new version of inertial navigation Moved several navigation functions from ArduCopter.pde to navigation.pde	12 years ago
rmackay9	a1b4ec6d0e	ArduCopter: move to use new INS library instead of IMU library	12 years ago
Jason Short	8a8ed7a711	ACM : Formatting	12 years ago
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.	12 years ago
rmackay9	5e8043fd9c	ArduCopter: changed ACRO_ROLL_STABILIZE and ACRO_PITCH_STABILIZE to parameters Changes on behalf of Leonard Hall	12 years ago
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	12 years ago
rmackay9	583f2e49a3	ArduCopter: integrated Leonard Hall's improved ACRO mode	12 years ago
rmackay9	b944d9df26	ArduCopter: bug fix in earthframe->body frame translation. Provided by Leonard Hall. Also removed large unnecessary comments.	12 years ago
rmackay9	5fbe53a84d	ArduCopter: bug fix for get_yaw_rate_stabilized_ef Provided by Leonard Hall	12 years ago
LeonardTHall	d7b7e1cefa	New Yaw controller using rate feed forward and stabilize. Signed-off-by: LeonardTHall <LeonardTHall@gmail.com>	12 years ago
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.	12 years ago
rmackay9	2848bb8ee6	ArduCopter: freeze I terms if motor limits breached	13 years ago
rmackay9	7cf60e61b4	ArduCopter: bug fix in earth-frame to body-frame conversion for roll	13 years ago
rmackay9	05fd04134a	ArduCopter: fix heli build	13 years ago
rmackay9	e375a27058	ArduCopter: prioritise rate controllers, rate controller targets converted to body frame	13 years ago
rmackay9	361ff0c08f	ArduCopter: allow PID logging of throttle. Make get_angle_boost actually use parameter passed in.	13 years ago
uncrustify	f783ace0de	uncrustify ArduCopter/Attitude.pde	13 years ago
Jason Short	0a25a189eb	ACM \| Attitude.pde - removed next_wp.alt reset.	13 years ago
Jason Short	bc631b656e	ACM: Added a more sane limit to Angle boost	13 years ago
rmackay9	87d5b5944d	ArduCopter: commented out get_acro_yaw2 function to reduce compiler warnings	13 years ago
rmackay9	92688a793a	ArduCopter: fixed compiler warning related to shadowing of control_roll and control_pitch in get_of_roll and get_of_pitch.	13 years ago
Jason Short	9cee1b2fa0	ACM : Upped Yaw Limit to 2200	13 years ago
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.	13 years ago
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.	13 years ago
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.	13 years ago
Jason Short	132ac7d412	ACM : attitude.pde - removed unused function	13 years ago
Jason Short	5d756decd2	ACM : Attitude.pde yaw limit, moved toy code out of att to it's own pre	13 years ago
Jason Short	8c47b0c087	ACM: Toy mode fix - Pitch flipped the sign on roll/Yaw coupling.	13 years ago
Jason Short	613849a8df	Arducopter: Force nav_yaw to match auto_yaw when starting a mission	13 years ago

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322 Commits (d618c55e2ff52c7fad943bbeca7b85a03b8079e5)