Matthias Grob
9ff9692270
mc_att_control: switch to quaternion attitude control (no yaw reduction yet)
2018-03-15 17:16:14 +01:00
Daniel Agar
1abf90c6d4
EKF2 only publish wind_estimate if wind velocity is being estimated
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- refactor body wind velocity calculation
2018-03-15 07:18:58 +01:00
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
Daniel Agar
f194c5424c
move hmc5883 i2c address into driver
2018-03-14 14:38:40 -04:00
Daniel Agar
bb7466c596
move rgbled i2c address into driver
2018-03-14 14:38:40 -04:00
Daniel Agar
de85acb8b0
px4fmu-v2 version detection and init cleanup
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- if an invalid version is detected reinit, then reset
2018-03-14 08:02:19 +01:00
Beat Küng
2bcc5cf3e5
imu filter defaults: set IMU_GYRO_CUTOFF to 80 and MC_DTERM_CUTOFF to 30
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tested on at least 5 different vehicles, including AeroFC. The values
should be conservative, good setups (with low vibrations) can increase
these values even further.
increasing IMU_GYRO_CUTOFF allows for better tuning gains (increased P).
2018-03-13 20:54:49 +01:00
Beat Küng
a99e49a856
landing_target_estimator: fix param type: int -> int32_t
2018-03-13 17:35:15 +01:00
Beat Küng
7ee464c264
LPE: refactor to use ModuleParams
2018-03-13 17:35:15 +01:00
Beat Küng
83d55773af
LPE: refactor to use ModuleBase
2018-03-13 17:35:15 +01:00
Beat Küng
9fb9b2916a
LPE: use default & delete keywords for constructors & destructors
2018-03-13 17:35:15 +01:00
Beat Küng
f7ee3c2015
cmake configs: add vtol_att_control for required parameters VT_B_DEC_MSS & VT_B_REV_DEL
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Required by Navigator.
2018-03-13 17:35:15 +01:00
Beat Küng
279b66bfbd
ekf2: use new Param class
...
reduces RAM usage by 1.3KB
2018-03-13 17:35:15 +01:00
Beat Küng
eb33145ac8
px4_param.h: add ParamExtFloat & ParamExtInt (required by ekf2)
2018-03-13 17:35:15 +01:00
Beat Küng
89a775b401
navigator: remove use of final to allow extending class hierarchy
2018-03-13 17:35:15 +01:00
Beat Küng
8a5cdac1f4
FixedwingPositionControl: fix ordering of PRINT_MODULE_USAGE_NAME
2018-03-13 17:35:15 +01:00
Beat Küng
e0af2912a1
navigator: avoid use of a static variable last_geofence_check
2018-03-13 17:35:15 +01:00
Beat Küng
320bdc6482
navigator: refactor to use ModuleBase class
2018-03-13 17:35:15 +01:00
Beat Küng
246be4f0ab
precland: use 'default' for destructor
2018-03-13 17:35:15 +01:00
Beat Küng
2e6904b8a4
navigator: use '#pragma once' as include guard
2018-03-13 17:35:15 +01:00
Beat Küng
f2dddc65a5
navigator: use new Param class
2018-03-13 17:35:15 +01:00
Beat Küng
32eaf278ad
Battery: remove unnecessary updateParams() call in constructor
2018-03-13 17:35:15 +01:00
Beat Küng
523bb11577
module template: update to use the new Param classes
2018-03-13 17:35:15 +01:00
Beat Küng
0d26aeafe2
px4_parameter.h: remove this file - it's not used anymore
2018-03-13 17:35:15 +01:00
Beat Küng
fca99cf775
param: refactor BlockParam classes
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- make the selected parameter a template argument. This
enables type-checking at compile-time.
- move things to src/platforms.
This provides consistent includes with ModuleBase
- add ModuleParams base class (replaces Block & SuperBlock)
- drop the Block* prefix from the class names
2018-03-13 17:35:15 +01:00
Beat Küng
0e4034d01e
param: add a px4_parameters_public.h.jinja template
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Generates an enum with all params & additional type information for static
type checking
The generated public param header is required to build the modules using
the new BlockParam classes.
2018-03-13 17:35:15 +01:00
Beat Küng
0a5af01454
NavigatorMode: inherit from Block instead of SuperBlock
2018-03-13 17:35:15 +01:00
Philipp Oettershagen
ff66605a8a
Fix: Increase pwmsim module stack by 100 bytes again because load_mon was giving warning about low stack
2018-03-13 12:51:33 +01:00
David Sidrane
de9368319f
Do not change mode to read temperature
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The mode change was not necessary and in fact caused the chip to not update the registerfile resulting in MAG timeouts
2018-03-12 11:56:59 +01:00
Beat Küng
bb6802a1ed
kinetis: fix PPM decoding
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On kinetis, the TPM_STATUS_TOF was used to detect missed interrupts for
PPM decoding. However this was not correct, because the TOF bit was set on
each timer overflow. This happened regularly after every 64ms interval,
which meant that most PPM frames were just discarded.
I have not found any equivalent register/solution that is used on STMF4,
so this just removes the TOF handling. However there is now no way to
detect missed edges/interrupts!
2018-03-12 11:56:59 +01:00
Beat Küng
5a7885610d
fmu: fix PPM publication if RC_SERIAL_PORT is not defined
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Before, the RC channel was published as fast as the fmu was running
(around 200Hz in unarmed state).
And fix code style.
2018-03-12 11:56:59 +01:00
Beat Küng
dde922a971
fxos8701cq: add a 'stop' command
2018-03-12 11:56:59 +01:00
David Sidrane
0ed631227f
fxos8701cq:Work with fxos8701cq and fxos8700cq
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Allow whoami of fxos8701cq and fxos8700cq
2018-03-12 11:56:59 +01:00
Daniel Agar
5335778f6e
nxphlite start correct sensors and disable debug
2018-03-11 18:19:12 -05:00
Mohammed Kabir
f95f4c5f09
UAVCAN : Correct startup sequence and improve parameter description
2018-03-10 23:09:19 -05:00
Vasily Evseenko
ebe74ccb2e
Add 'forced on' flow control mode to mavlink UART ( #8776 )
2018-03-10 14:54:57 -05:00
acfloria
fd0be3c412
Remove MavLink dependency in navigator
2018-03-09 21:16:28 +01:00
Roman
64b97cb18e
fw_att_control: in acro use thrust from rate setpoint topic
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-09 13:48:14 +01:00
Thomas Stastny
74730273c1
fw_att_control move angular rate limits to body angular rates ( #9023 )
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* ecl: attitude_fw update
- move angular rate limits to body angular rates
- handle rattitude/acro vs attitude mode rate limits
2018-03-08 22:55:45 -05:00
Daniel Agar
2ce8b6a984
delete VT_FW_PITCH_TRIM parameter ( #9014 )
2018-03-07 09:08:59 -05:00
Roman
ac2b3ccadc
vtol_att_control: default front transition throttle to 100%
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- the main idea is to prevent airspeed less systems to stall after a
transition
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
e4ea7262fd
tailsitter.cpp: small cosmetic fix
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
03338935e0
vtol_att_control: make sure blending airspeed is smaller than transition airspeed
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
e0ca38e794
standard vtol: fix mc weight calculation
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
23257bf6ee
standard vtol: simplify blending weight calculation
...
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
b66bc712af
tailsitter: avoid doing same calculation twice
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
1d8f588d37
vtol_att_control: switch from division to multiplication for variable
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calculation
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00
Roman
9e16543dbe
tiltrotor: represent time since transition in seconds
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- more intuitive
- avoids tons of divisions
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-07 14:01:51 +01:00