Robert Lefebvre
fa24107a2a
AP_MotorsHeli_RSC: Split out rotor speed estimate into it's own function
2015-10-10 15:11:40 +09:00
Robert Lefebvre
9e8f5a42f4
AP_MotorsHeli: Colyaw function to check if rotor speed control is above idle
2015-10-10 15:11:37 +09:00
Robert Lefebvre
d788f0307d
AP_MotorsHeli: rework RSC output() function to implement idle speed function
...
Also, split out speed_ramp function
2015-10-10 15:11:35 +09:00
Robert Lefebvre
b879b312e9
AP_MotorsHeli_Single: Fix recalc_scalars function
2015-10-10 15:11:32 +09:00
Robert Lefebvre
24244ba576
AP_MotorsHeli: Create RSC_IDLE param
2015-10-10 15:11:30 +09:00
Robert Lefebvre
718397c772
AP_MotorsHeli: Change RSC output() function into a state machine.
2015-10-10 15:11:27 +09:00
Robert Lefebvre
bf0fd3b3f2
AP_MotorsHeli: Fully detail tradheli output functions and move manual servo handling
2015-10-10 15:11:25 +09:00
Robert Lefebvre
ec400e06d8
AP_MotorsHeli: Rename tradheli servo objects for clarity
2015-10-10 15:11:22 +09:00
Robert Lefebvre
6a7996d367
AP_MotorsHeli: Update includes so that it builds
2015-10-10 15:11:19 +09:00
Fredrik Hedberg
d1fbf739c0
AP_Motors: Fix param indices in AP_MotorsHeli.
2015-10-10 15:11:16 +09:00
Fredrik Hedberg
260d018db9
AP_Motors: Rename output_yaw to move_yaw in AP_MotorsHeli_Single.
2015-10-10 15:11:13 +09:00
Fredrik Hedberg
7ac02922e9
AP_Motors: Fix formatting in AP_MotorsHeli_RSC.
2015-10-10 15:11:10 +09:00
Fredrik Hedberg
fae1dcc42b
AP_Motors: Fix param range comment in AP_MotorsHeli.
2015-10-10 15:11:08 +09:00
Fredrik Hedberg
cde94078b7
AP_Motors: Move traditional helicopter controls into AP_MotorsHeli_Single.
...
Original commit by fhedberg, had to fix merge conflicts and now it appears I did the commit?
2015-10-10 15:11:03 +09:00
Fredrik Hedberg
af1eee44ee
AP_Motors: Break out yaw output in AP_MotorsHeli.
2015-10-10 15:11:00 +09:00
Fredrik Hedberg
ded265dbe1
AP_Motors: Break out servo init and reset in AP_MotorsHeli.
2015-10-10 15:10:57 +09:00
Fredrik Hedberg
54452e2a74
AP_Motors: Move rotor speed control into AP_MotorsHeli_RSC.
2015-10-10 15:10:53 +09:00
Fredrik Hedberg
e360b21b2a
AP_Motors: Use C++11 initializers in AP_MotorsHeli.
2015-10-10 15:10:50 +09:00
Paul Riseborough
5aa6dc5a01
AP_NavEKF: Ensure bad mag data cannot cause the heading to reset too often
2015-09-16 15:16:09 +09:00
Paul Riseborough
efce10b6cd
AP_NavEKF: Reset mag and heading states to try and pass pre-flight checks
2015-09-16 15:16:08 +09:00
Randy Mackay
72ab60a19e
AP_Compass: fix consistent check for less than three compasses
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Also use vector functions where available
2015-09-16 15:15:18 +09:00
Jonathan Challinger
2f4f76d17a
AP_Compass: add consistent() function
2015-09-16 15:14:53 +09:00
Randy Mackay
a0906188b3
Math: add Vector2 is_zero method
2015-09-16 15:14:47 +09:00
Andrew Tridgell
08e1a66772
APM_OBC: added severities to send_statustext_all
2015-09-10 15:09:54 +09:00
Andrew Tridgell
33248b00d4
AP_NavEKF: only call calcGpsGoodToAlign if we need to
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avoid calling it once we have an origin. This avoids some calculations
and string operations
2015-09-10 14:51:47 +09:00
Andrew Tridgell
c4d561a4eb
AP_NavEKF: added prearm_failure_reason()
2015-09-10 14:51:25 +09:00
Andrew Tridgell
c93006dc15
AP_AHRS: added prearm_failure_reason()
2015-09-10 14:51:22 +09:00
Andrew Tridgell
c268cea08f
GCS_MAVLink: added severity to send_statustext_all()
2015-09-10 14:51:19 +09:00
Andrew Tridgell
55e6008e38
GCS_MAVLink: make send_statustext_all() take a format string
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this allows for formatted messages to all groundstations in libraries
2015-09-10 14:51:13 +09:00
Paul Riseborough
78ac1340c8
AP_NavEKF: Prevent false triggering of optical flow takeoff detection
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Now that we have a pre-arm check in place to detect bad lidar, the motion check is unnecessary and can false trigger for copters with flexible undercarriages or on uneven ground.
2015-08-28 12:04:36 +09:00
Randy Mackay
13e360df08
Mission: sanity check location
2015-08-28 12:04:32 +09:00
Randy Mackay
f3590120a5
BattMonitor: fix parameter descriptions
2015-08-28 12:04:24 +09:00
fillycheezstake
b618621303
Mount: fix for STORM32 serial ver 78e and higher
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This fixes the structs to be compatible with the changes OlliW made to
the gimbal firmware.
http://www.olliw.eu/storm32bgc-wiki/Serial_Communication
2015-08-28 12:04:22 +09:00
Leonard Hall
9dfe30f514
Copter: increase default thrust expo to 0.65
2015-08-28 12:04:21 +09:00
Randy Mackay
9cd5e4dd6b
AC_WPNav: remove unused get_wp_radius
2015-08-28 12:04:16 +09:00
squilter
d00f9b61b4
GCS_MAVLink: make arguments mandatory for send_autopilot_version
2015-08-28 12:04:12 +09:00
squilter
8553301cdd
GCS_MAVLink: send_autopilot_version accepts version
2015-08-28 10:27:00 +09:00
Randy Mackay
7299011510
GCS_MAVLink: version update after common.xml change
2015-08-28 10:26:57 +09:00
squilter
de712714ef
GCS_MAVLink: regenerate common
2015-08-28 10:26:55 +09:00
Randy Mackay
730e4908a9
GCS_MAVLink: rename FIRMWARE_VERSION_TYPE and fully qualify items
2015-08-28 10:26:52 +09:00
squilter
f3f11a4e96
GCS_MAVLink: Add FIRMWARE_RELEASE_TYPE to common.xml
2015-08-28 10:26:49 +09:00
Tom Pittenger
04000faa5f
AP_InertialSensor: correct USE param storage index
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USE, USE2, USE3 have 20, 21, 21 but should be 20, 21, 22
2015-08-28 10:26:21 +09:00
Randy Mackay
bf584af9b0
NavEKF: use maxf when retrieving vibration levels
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This reduces the performance hit that was caused by multiple calls to get_vibration_levels
2015-08-19 20:45:13 +09:00
Randy Mackay
f61c62b44a
Math: maxf and minf functions
2015-08-19 20:45:12 +09:00
Randy Mackay
0ea47ea7b8
NavEKF: IMUSwitchState enum
2015-08-19 20:45:11 +09:00
Randy Mackay
32c7fe996a
NavEKF: IMU ratio set to primary accel when neither IMU is used
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This forces the EKF IMU ratio to indicate which IMU is used except that it will be "0" in the unlikely case that the third IMU is used
2015-08-19 20:45:10 +09:00
Paul Riseborough
77cac09bf6
AP_NavEKF: Add hysteresis to IMU switching logic
2015-08-19 20:45:09 +09:00
Paul Riseborough
e4a4dc26c8
AP_NavEKF: Modify method used to check for vibration errors
...
This method checks for consistency between accelerometer readings and switches to the unit with the lowest vibration of the difference exceeds 0.3g
The threshold of 1.7 m/s/s corresponds to a maximum tilt error of 10 deg assuming one IMU is good, one is bad and the EKF is using the bad IMU.
2015-08-19 20:45:07 +09:00
Randy Mackay
e2c8d6eb9d
AHRS_NavEKF: integrate INS use_accel
2015-08-19 20:45:06 +09:00
Randy Mackay
437074a8fb
AHRS_DCM: integrate INS use_accel
2015-08-19 20:45:05 +09:00
