Commit Graph
593 Commits
Author SHA1 Message Date
Timothy Scott a134da6e12 Removed is_rotor_wing, replaced with vehicle_type 2019-06-13 10:04:26 +02:00
Daniel Agar 4bef573497 fw_pos_control_l1 move to new uORB::Subscription 2019-06-06 20:00:02 -04:00
Daniel Agar 2c63e335e9 uORB::Subscription subscribe directly to uORB device node object 2019-06-03 17:06:21 -04:00
Daniel Agar bf12583d80 fw_pos_control_l1 replace FW_LND_THRTC_SC param description < character
- fixes #12124
2019-05-30 18:03:03 -04:00
Julian Oes 2ac8841f35 vtol/fw/mc: fix VTOL enum shadowing
This changes the enums used for various VTOL states to enum classes
which makes them type-safe and should avoid shadowing.

This change was motivated by a Clang warning about shadowing of the
enum const TRANSITION_TO_FW which was declared twice, once in
vtol_type.h and once in standard.h.

This change only removes the shadowing but presumably these enums could
be cleaned up and consolidated further.
2019-05-29 23:51:10 -04:00
Daniel Agar 9bad61b86b Improve robustness to bad and lost airspeed data (#11846) 2019-04-30 03:08:23 -04:00
Roman 2bd8b517c5 FwPositionControl: don't do takeoff help for vtol
- takeoff help is used for fixed wings, it increases the altitude setpoint
after a launch. A vtol does not need this as it's already sufficiently
high up in the air.

Signed-off-by: Roman <bapstroman@gmail.com>
2019-04-30 02:45:49 -04:00
Daniel Agar d36b06f779 fw_pos_control_l1: FW_LND_EARLYCFG disable by default
- change to boolean param
2019-04-13 17:35:12 +02:00
bresch 10ba0801d2 Parameter update - Rename variables in modules/fw_pos_control
using parameter_update.py script
2019-04-03 15:38:50 +02:00
Daniel Agar ec3bc4ee5b fw_pos_control_l1 reset internal takeoff and landing state when arming 2019-04-03 08:48:30 +02:00
Daniel Agar 45d7165eb3 fw_pos_control_l1 skip wind > max airspeed logic if airspeed invalid
- cleanup airspeed validity check logic
2019-01-12 14:19:53 +01:00
Daniel Agar 60f2a92e3d replace <cfloat> with <float.h>
- <cfloat> isn't available in the NuttX c++ library
2019-01-06 19:20:57 -05:00
Alvar Martti 63651da309 FW bug in checking if landing point has been passed
* the bearing difference between the waypoints and aircraft to landing point should be wrap_pi'ed
2018-12-21 10:03:31 -08:00
Roman Bapst 90bfdb6f0a VTOL rate control architecture improvements (#10819)
* attitude and rate setpoint message: use 3D array for thrust demand
* FixedWingAttitudeControl: rework airspeed scaling
  * move airspeed and scaling calculation into separate method
  * if vtol in hover and airspeed disabled use minimum airspeed instead of trim airspeed
2018-11-21 20:32:40 -05:00
Hamish Willee 44f650fdc9 Add additional info to FW_LND_USETER (#10777) 2018-10-30 10:14:52 -04:00
CarlOlsson 82106cc4c1 fw_l1_control: add underscores to perf for consistency 2018-10-22 09:26:06 -04:00
Roman e17f0802cc tecs msg: changed flight_path_angle to height rate as clearly we are
looking at height rates

Signed-off-by: Roman <bapstroman@gmail.com>
2018-09-17 10:27:08 -04:00
Daniel Agar a6dabbbae7 Landing slope move to standalone library
- this is shared by both the FW position controller and navigator's
   missiong feasibility checker
2018-08-31 14:43:51 -04:00
Daniel Agar 5207c420c3 generic position controller status/feedback message 2018-08-31 14:43:51 -04:00
Philipp Oettershagen c997159e32 Fixed-wing autoland: Introduce parameter to enable/disable the early activation of the landing configuration 2018-08-24 10:13:07 -04:00
Philipp Oettershagen 953cff7ba0 Fixed-wing autoland: Parameter description fixes 2018-08-24 10:13:07 -04:00
Philipp Oettershagen 20c02ae093 Fixed-wing autoland: Adapt according to @dagar's and @antiheavy's comments. 2018-08-24 10:13:07 -04:00
Philipp Oettershagen 08ceddaddb Fixed-wing autoland: ALWAYS flare when close to the ground, independently of the horizontal distance to the land WP. This avoids that we crash into the ground at negative pitch and guarantees that the flare always starts at the same altitude above ground. However, the motor shutoff still depends on the horizontal distance to the LAND WP, thus avoiding that the motor is shut off prematurely 2018-08-24 10:13:07 -04:00
Philipp Oettershagen 4c4f585ad5 Fixed-wing autoland: 1) The landing configuration (flaps, different airspeed) is now already set during the loiter down instead of at the start of the landing approach. This is done to avoid any mode changes (which can cause altitude/airspeed jumps) so close to the gorund. 2) A scaling factor for the TECS throttle time constant was added which allows tighter throttle control during the landing (i.e. close to the ground) than high up in the air 2018-08-24 10:13:07 -04:00
Roman Bapst 8b1381ead9 update ecl l1 and usage for new roll angle setpoint slew rate limit (#10005)
* added ability to slew rate limit the roll angle output of the l1 controller
* FixedWingPositionControl: this avoids the steps in roll angle setpoint which occur when the controller
switches to a new waypoint
* GroundRoverPositionControl: adapted to new l1 API
2018-08-01 14:01:41 -04:00
TSC21 ca42483794 update msgs fields from camelCase to snake_case so rosidl_generate_interfaces() is able to generate code for ROS IDL files 2018-07-30 21:40:28 +02:00
Daniel Agar 9a4de09325 sensors remove airspeed negative check 2018-07-16 01:09:19 -04:00
Thomas Stastny 8a7919bcb6 fw att+pos ctrl: use enum for flaps configs 2018-07-11 08:08:13 +02:00
Thomas Stastny 0c3399433d fw att+pos ctrl: add takeoff flaps setting 2018-07-11 08:08:13 +02:00
Daniel Agar 9fa882119d fw_pos_ctrl_l1 remove unnecessary orb rate limits 2018-07-05 12:16:44 -04:00
Philipp Oettershagen 6579b7254a Change TECS max sink rate minimum value, because very fragile aircraft might not be able to sustain higher max sink rates 2018-07-01 10:42:27 -04:00
Philipp Oettershagen a76c4c55d4 Decrease default flare altitude. The previous value was way too high for any small aircraft. It was also unsafe because after the flar, pitch is currently controlled open-loop, which means that stall can potentially happen during the flare 2018-07-01 10:42:27 -04:00
Philipp Oettershagen 8f09a20478 Update TECS integrator gain parameter description to represent the changes in https://github.com/PX4/ecl/commit/ccfba4997147658d8340f7efa351c19299120704 2018-07-01 10:42:27 -04:00
Daniel Agar cf74166801 double promotion warning fix or ignore per module 2018-07-01 09:36:55 +00:00
Philipp Oettershagen 753ad0e0df Fixed-wing autoland: Fix bug that could cause a steep pitch increase and thus aircraft stall during the flare (#9674) 2018-06-14 11:29:03 -04:00
Daniel Agar 222a91c6be mathlib delete Matrix, Quaternion, Vector 2018-05-23 17:27:09 -04:00
Daniel Agar 2e92484325 ecl update to latest master with separate libraries (#9406) 2018-05-03 23:48:09 -04:00
Daniel Agar ea3acb7121 cmake remove circular linking and reorganize
- px4_add_module now requires MAIN
 - px4_add_library doesn't automatically link
2018-04-29 21:48:54 -04:00
Daniel Agar 0e823c82b6 FW landing check if prev valid before using (#9284) 2018-04-21 12:03:46 -04:00
Daniel Agar d75fd72c02 stop manually defining physical constants 2018-04-19 07:24:58 +02:00
Roman 0f1c9504d5 FixedWingPositionControl: rotate attitude consistenly for tailsitters
Signed-off-by: Roman <bapstroman@gmail.com>
2018-04-18 16:20:15 +02:00
Daniel Agar a78ab02144 fw_pos_control_l1 don't store TECS and L1 parameters 2018-04-12 00:46:49 -04:00
Daniel Agar 29b3950747 move geo and geo_lookup to PX4/ecl 2018-03-26 23:16:55 -04:00
Beat Küng b512d11e54 refactor fw_pos_control_l1: replace BlockParam* with Param* classes
Also change naming convention: add _ prefix to class attributes
2018-03-22 08:19:08 +01:00
sanderux d87b7ac7f4 Fix scale application on FW throttle baro compensation 2018-03-20 00:13:36 +01:00
Daniel Agar b6b7fddb9f TECS and L1 switch to matrix math library (#9101) 2018-03-19 18:09:54 -04:00
Daniel Agar 7607c71ca8 fw_pos_control_l1 project virtual waypoint to handle landing overshoot 2018-03-14 16:39:19 -04:00
Daniel Agar d1dca4e74c fw_pos_ctrl_l1 move takeoff to control_takeoff() 2018-03-14 16:39:19 -04:00
Daniel Agar c72340e039 fw_pos_ctrl_l1 move landing to control_landing() 2018-03-14 16:39:19 -04:00
Beat Küng 8a5cdac1f4 FixedwingPositionControl: fix ordering of PRINT_MODULE_USAGE_NAME 2018-03-13 17:35:15 +01:00