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
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
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reduces RAM usage by 1.3KB
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
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
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
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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
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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
Roman
ae2e6c7a18
tailsitter: 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
Roman
bf22f02567
tailsitter: removed usage of hrt_elapsed and small cleanup
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- do not call hrt_elapsed_time since it's expensive
- remove P2 front transition phase (was not even used)
Signed-off-by: Roman <bapstroman@gmail.com>
2018-03-07 14:01:51 +01:00
Roman
196d0e40b4
standard vtol: use time in second since transition start instead of using
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microseconds
- seconds is more intuitive
- avoids tons of divisions by 1e6f
Signed-off-by: Roman <bapstroman@gmail.com>
2018-03-07 14:01:51 +01:00
Roman
5a2a5127fa
tailsitter: removed common vtol parameters
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Signed-off-by: Roman <bapstroman@gmail.com>
2018-03-07 14:01:51 +01:00
Roman
07a84f2246
tiltrotor: removed common vtol parameters
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Signed-off-by: Roman <bapstroman@gmail.com>
2018-03-07 14:01:51 +01:00
Roman
6900f97b72
vtol_att_control: use airspeed_disabled flag instead of airspeed mode
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Signed-off-by: Roman <bapstroman@gmail.com>
2018-03-07 14:01:51 +01:00
Roman
daa6c6ffc8
vtol_att_control: consolidated standard parameters & fix usage of hrt_elapsed time
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- standard vtol was implementing many custom parameters although they
are generic and should be shared between the vtol types
- removed heavy usage of hrt_elapsed_time() which is a system call and
could be computationally expensive
2018-03-07 14:01:51 +01:00
Julian Oes
9c6b1a0f04
navigator: fix incorrect takeoff altitude
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This fixes a problem where we do not properly go to the set takeoff
altitude but end up lower.
The problem was that the setpoint triplet is reset when the navigation
mode changes. So in this case, the triplet is reset when we switch from
takeoff to loiter which can happen before reaching the actual takeoff
altitude.
The fix is an ugly hack to prevent the reset in the case of takeoff to
loiter. A better solution would be to remove the general reset and have
all navigation modes do the proper resets themselves.
This hotfix should however be lower risk.
2018-03-07 08:48:44 +01:00
Daniel Agar
623e16e8be
logger SITL add additional messages by default
2018-03-06 17:42:33 +01:00
AlexKlimaj
83d01a7c76
Updated batt_smbus. Expanded battery_status.msg. Fixed mavlink_messages.cpp temperature. ( #8991 )
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* Updated and expanded batt_smbus to work with bq40z50-R2. Expanded battery_status.msg. Fixed mavlink_messages.cpp temperature, added commented out expanded battery_status.msg parameters for future mavlink expansion.
* Changed errx to PX4_ERR
* Added PX4_ERR returns
2018-03-06 10:42:20 +01:00
Daniel Agar
493c41c76e
VtolLandDetector require vehicle_status timestamp
2018-03-05 15:46:24 -05:00
Daniel Agar
354584acfc
MulticopterLandDetector initialize all class members
2018-03-05 15:46:24 -05:00
Daniel Agar
69470f6991
land_detector use THROTTLE index
2018-03-05 15:46:24 -05:00