Commit Graph
502 Commits
Author SHA1 Message Date
Daniel Agar a41001354a FW landingslope delete unused (#7046) 2017-04-13 18:18:57 -04:00
Daniel Agar 0b8e88f476 fw_pos_control_l1 remove unnecessary ground_speed 2017-04-10 09:41:01 +02:00
Daniel Agar dc30498c80 fw_pos_control_l1 control_position split position_setpoint_triplet 2017-04-10 09:41:01 +02:00
Daniel Agar 0b0c552dee fw_pos_control_l1 remove unused ground_speed arg 2017-04-10 09:41:01 +02:00
Daniel Agar af7b2cd22f fw_pos_control_l1 cleanup init and uorb helpers 2017-04-10 09:41:01 +02:00
Daniel Agar 474ce2851e fw_pos_control_l1 using math constrain, max, min, radians 2017-04-10 09:41:01 +02:00
Daniel Agar 8b4877a6eb fw_pos_control_l1 delete unused terrain helper 2017-04-10 09:41:01 +02:00
Daniel Agar c5e0bf1c2f uORB combine VTOL FW and MC virtual topics (#7008) 2017-04-09 13:17:20 -04:00
Daniel Agar a6eb0053c5 TECS default FW_T_HRATE_FF 0.8 2017-04-05 09:31:20 +02:00
Daniel Agar 22d0e507c6 TECS fix height demand change 2017-04-05 09:31:20 +02:00
Daniel Agar 4b8bedef48 avoid double promotions 2017-04-01 20:19:28 +02:00
Daniel Agar ecb2511a7b add matrix copyTo 2017-02-25 11:04:02 +01:00
aivian 7a77e27a79 fixed wing offboard attitude setpoint fix (#6112) 2017-02-15 23:51:50 -05:00
Daniel Agar ff68d63143 fw_pos_control_l1 force heading hold at flare 2017-02-12 11:03:51 +01:00
Daniel Agar 94d6a92f41 fw_pos_control_l1 publish quat in att_sp 2017-02-12 11:03:51 +01:00
Daniel Agar e927f3e040 clang-tidy modernize-use-nullptr 2017-02-01 22:15:50 -05:00
Daniel Agar 830cb44b9c astyle src/modules/fw_pos_control_l1 2017-01-29 01:18:32 +01:00
Lorenz Meier 0e09f072e1 L1: Header cleanup 2016-12-27 21:00:51 +01:00
Roman a61b1e089c make sure to update the reset counters every time the topic updates
Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman 76f862de33 fw_pos_control_l1: when doing a position reset just reset position controller
- do not try to shift the target waypoints when a reset occurs in position
control mode. Just make it lock into the current heading.

Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman 7ba49aeb80 fw_pos_control_l1: make TECS handle height ekf height resets properly
Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman 8155044b40 fw_pos_control_l1: put comments for lat/lon wrapping
Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman f80b4f8732 fw_pos_ctrl_l1: added wrapping of lat lon coordinate after addition of
delta reset

Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman b3f9114b1c fw_pos_control_l1: added missing alitude reset counter update
Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
Roman d4c87d62f1 fixed code style
Signed-off-by: Roman <bapstroman@gmail.com>
2016-11-21 07:29:21 +01:00
tumbili b2410460a5 made position controllers handle estimator state resets 2016-11-21 07:29:21 +01:00
Daniel Agar a8369c6ac8 FW use loiter to achieve waypoint altitude
- fixes #5061
2016-11-05 10:30:36 +01:00
Beat Küng 241fd629ce ERROR macro: get rid of the many 'oddly, ERROR is not defined for c++', use PX4_ERROR 2016-09-30 13:50:51 +02:00
Lorenz Meier 17a1d31b79 Update L1 controller stack 2016-09-30 09:16:36 +02:00
Julian Oes 8ff237c69f Remove size optimization for individual modules
It makes more sense to set the optimization flags on a platform basis
instead of individually for each module. This allows for different
optimization options for SITL, NuttX, Snapdragon, etc.
2016-09-30 08:11:51 +02:00
Daniel Agar fb75240ee9 FW init TECS with PSP_OFF and constrain TAS error 2016-09-27 08:49:45 +02:00
Daniel Agar 9fd0513be3 vtol remove unused vehicle_status 2016-09-27 08:49:45 +02:00
Roman ab4731a99f fw_pos_control_l1: for tailsitters we need to rotate the body acceleration
vector as it has it's reference in the mc frame

Signed-off-by: Roman <bapstroman@gmail.com>
2016-09-13 14:32:00 +02:00
Daniel Agar 2a15578f8d FW implement MAV_CMD_DO_GO_AROUND 2016-08-06 20:56:53 +02:00
Beat Küng aefa319fc4 fw_pos_control_l1: fix compiler problem (implicit float conversion) (#5198)
issue (GCC 6.1.1):
../src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp:1284:27: error: implicit conversion from ‘float’ to ‘double’ to match other operand of binary expression [-Werror=double-promotion]
  if ((fabs(air_gnd_angle) > M_PI) || (ground_speed_2d.length() < 3.0f)) {
2016-08-02 00:04:44 -07:00
Daniel Agar 2de66b1a9d FW navigation in high winds (#5097) 2016-07-29 06:05:48 -07:00
sander 0ce08ed9f8 Code style 2016-07-28 16:44:27 +02:00
sander ce3749d04f Make tecs init airspeed mode dependent 2016-07-28 16:44:26 +02:00
sander 0cf77a30b1 Init tecs with transition airspeed for vtols without airspeed sensor 2016-07-28 16:44:26 +02:00
Andreas Antener 50175ca7ea manual condition includes threshold values 2016-07-25 08:56:19 +02:00
Roman aea7bd5b47 fw_attitude_control: calculate attitude setpoint for STAB mode
- attitude setpoint generation for stabilized mode was shifted back
to the fw attitude controller. since the fw position controller is polling
on global position attitude setpoints were not generated when global
position was not published.

Signed-off-by: Roman <bapstroman@gmail.com>
2016-07-25 08:56:19 +02:00
Andreas Antener 254358ef86 fixed implicit conversion 2016-07-25 08:56:19 +02:00
Andreas Antener 89a2f5057f fixed code style 2016-07-25 08:56:19 +02:00
Andreas Antener 6ff65cd8b2 reset attitude setpoint where necessary 2016-07-25 08:56:19 +02:00
Andreas Antener 0a997577f5 allow manual yaw in all manual modes and also use it as threshold to snap into heading lock 2016-07-25 08:56:19 +02:00
Andreas Antener 9f7f6e4d3d removed roll lock for altitude hold 2016-07-25 08:56:19 +02:00
Roman 6226a0c77d fw_pos_control_l1: fixed code style
Signed-off-by: Roman <bapstroman@gmail.com>
2016-07-25 08:56:19 +02:00
Roman ec334f7c9b fw_pos_control_l1: limit max roll and pitch setpoints for manual modes
Signed-off-by: Roman <bapstroman@gmail.com>
2016-07-25 08:56:18 +02:00
tumbili 8c8120e2fc fw position controller: logic cleanup
cleaned up logic when not to use pitch setpoint from TECS

Signed-off-by: tumbili <roman@px4.io>
2016-07-25 08:56:18 +02:00
tumbili fd51bf44d5 fw position / fw attitude control: move attitude setpoint generation to
position controller

- attitude setpoints for all modes are now computed in the fw position
controller

Signed-off-by: tumbili <roman@px4.io>
2016-07-25 08:56:18 +02:00