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
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
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
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
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
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
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
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
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
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
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
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
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
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
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
623e16e8be
logger SITL add additional messages by default
2018-03-06 17:42:33 +01:00
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
493c41c76e
VtolLandDetector require vehicle_status timestamp
2018-03-05 15:46:24 -05:00
354584acfc
MulticopterLandDetector initialize all class members
2018-03-05 15:46:24 -05:00
69470f6991
land_detector use THROTTLE index
2018-03-05 15:46:24 -05:00
458db2e508
vehicle_global_position remove redundant evh and evv
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- vehicle_status_flags condition_global_velocity_valid is also unnecessary
2018-03-05 13:20:28 -05:00
b9081fb0ab
vehicle_global_position delete unused pos_d_deriv
2018-03-05 01:41:18 -05:00
2f96dbb216
gnd_att_control param fix incorrect FW metadata
2018-03-04 18:23:12 -05:00
5ef27c5425
mavlink add minimal mode ( #8947 )
2018-03-04 17:50:28 -05:00
e340f6fd7a
FixedwingPositionControl: fix air_gnd_angle judgement condition.
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air_gnd_angle is from acos(), and never return a value that bigger than
M_PI_F
2018-03-02 21:57:11 +01:00
d39a8b5a48
Battery: Switch thrust based load compensation back to linear
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To account for the parameter definition.
My tests if quadratic is actually better in practise were anyways not conclusive.
2018-03-02 21:07:09 +01:00
5bb9babc20
Mavlink: round battery percentage up instead of down
2018-03-02 16:18:52 +01:00
4c4f990b3b
EKF2 remove FW_ARSP_MODE check
2018-03-02 08:58:08 +01:00
2ef9c4ec35
VTOL force land even when transitioning to FW ( #8958 )
2018-03-01 16:51:50 -05:00
3b0b5645e1
vtol_att update poll fd before poll call
2018-03-01 18:27:57 +01:00
ea3586cfd9
tailsitter: stop fiddling with thrust during transition and just let
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the mc pos controller handle it for now
Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-01 12:16:27 -05:00
08534588cd
fw_pos_control: get vtol parameter values if vehicle is vtol
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-01 12:16:27 -05:00
ee2163ce69
vtol_att_control: prevent segfault when no command line args given
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-03-01 11:35:34 -05:00
198708ba2e
rotation: updated board rotation meta data
2018-02-28 10:08:58 +01:00
40675bd1f4
logger: fix potential semaphore counter overflow
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When the timer callback is called at a higher rate than the logger can
execute the main loop (which is never the case under normal conditions),
the semaphore counter will increase unbounded, and eventually lead to
an assertion failure in NuttX.
The maximum semaphore counter is 0x7FFF, and when the logger runs at
default rate (3.5ms), the logger task must be blocked for 0x7FFF*3.5/1000
= 114 seconds continuously for an overflow to happen.
I see 2 cases where that could happen:
- the logger execution blocks somehow, or busy-loops in an inner loop
- a higher-prio task runs busy and hogs the CPU over a long period of time
2018-02-27 21:01:29 +01:00
611ab577d8
Battery: Fix estimate initialization
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On the Intel Aero and probably also other specific platforms
the first measured voltage values despite connected battery are unuasable.
The solution here is to start filtering and determining warning
only after a measurement above 2.1V was received.
2018-02-24 16:27:44 +01:00
83ac74367c
Battery: move member initialization values to class declaration
2018-02-24 16:27:44 +01:00
3917eb2d00
mavlink: don't send wrong time
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This prevents the autopilot from sending an invalid unix timestamp.
Usually, if no time is set yet by a GPS, the date is somehow set
to 2000-01-01, therefore we can ignore anything earlier than 2001.
2018-02-23 16:14:02 +01:00
df7364d2e2
Battery: Correct unit for capacity parameter
2018-02-23 15:30:17 +01:00
2549b702f0
pwm_out_sim, simulator_mavlink: fixed code style
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-02-22 15:10:22 -05:00
10bf6a4b59
params cmd: be less verbose
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-02-22 15:10:22 -05:00
ddb2dd89db
simulator mavlink: support for quad tiltrotor mav type
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Signed-off-by: Roman <bapstroman@gmail.com >
2018-02-22 15:10:22 -05:00
4cac6d1a44
tune_control: added define for tune strength
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This adds a define for the tune strength instead of hard-coding it with
a magic number.
2018-02-22 15:24:46 +01:00
19e706fede
fw_att_control fix attitude setpoint publication
2018-02-21 21:07:29 -05:00
a0f115b9ae
fw_att_control consolidate flaps code
2018-02-21 21:07:29 -05:00
4cb71f209f
fw_att_control centralize manual setpoint generation
2018-02-21 21:07:29 -05:00
7fa858ad84
fw_att_control only store battery_status scale
2018-02-21 21:07:29 -05:00
94b8e4a2bf
fw_att_control remove commented warnings
2018-02-21 21:07:29 -05:00
dcc47020a4
fw_att_control update params before poll
2018-02-21 21:07:29 -05:00
bf42964432
fw_att_control don't store entire vehicle_land_detected message
2018-02-21 21:07:29 -05:00
Roman