Randy Mackay
08f8fdfabd
Rover: report gyro unhealthy if failed calibration
2014-10-09 10:00:19 +09:00
Randy Mackay
6d8e760582
Plane: report gyro unhealthy if failed calibration
2014-10-09 10:00:17 +09:00
Randy Mackay
a8733ae8a8
Copter: support pre-flight calibration of gyro
2014-10-09 10:00:15 +09:00
Randy Mackay
9a0a83f404
Copter: report gyro unhealthy if failed calibration
2014-10-09 10:00:12 +09:00
Randy Mackay
128058362b
Copter: pre-arm check that gyro cal succeeded
2014-10-09 10:00:09 +09:00
Randy Mackay
834f2bea07
INS: add gyro_calibrated_ok_all method
...
This returns true if the gyros have been calibrated successfully
2014-10-09 10:00:07 +09:00
Andrew Tridgell
70ca87c4e6
AP_RangeFinder: handle all I2C rangefinder types on PX4 in PX4Firmware
2014-10-09 11:06:16 +11:00
Andrew Tridgell
49fa887773
Rover: prepare 2.47beta1
2014-10-09 09:20:11 +11:00
Andrew Tridgell
cebfef3ead
HAL_Linux: don't accept less than 5 input channels
2014-10-09 09:19:35 +11:00
Andrew Tridgell
1721216019
Rover: fixed skid steering
...
the main issue was the use of the last throttle in the throttle slew
rate control, but manual skid steering was also broken
2014-10-09 08:59:26 +11:00
Randy Mackay
8eba55ed67
Copter: throttle zero debounce to separate function
...
Also initialise throttle_zero to true on startup
Treat throttle less than zero as zero
2014-10-08 21:52:16 +09:00
Jonathan Challinger
8e3d163c3d
Copter: Change all zero throttle checks that should be conservative to use ap.throttle_zero
2014-10-08 20:54:24 +09:00
Jonathan Challinger
96f50b7cd7
Copter: add throttle_zero state
2014-10-08 20:54:19 +09:00
Jonathan Challinger
fa9d10e59b
Copter: log CURR message at 10hz
2014-10-08 20:49:36 +09:00
Andrew Tridgell
b0c9e97181
Linux_HAL_Essentials: P8.15 is an input pin
2014-10-08 12:50:50 +11:00
Andrew Tridgell
a3fee16604
HAL_Linux: added DSM/Spektrum RCInput support
...
this decodes DSM using the RCIN pulses from the PRU
2014-10-08 12:50:50 +11:00
Andrew Tridgell
3e3f87188b
HAL_Linux: enable DSM power pin
2014-10-08 12:50:50 +11:00
Andrew Tridgell
50e5ae6f7a
HAL_Linux: added low level DSM decoder
...
based on dsm.c from PX4 project
2014-10-08 12:50:50 +11:00
Craig Elder
adf741b959
Frame_params: Updated 3DR_X8-M_RTF.param
2014-10-07 15:00:57 -07:00
Randy Mackay
2f3f1a1d5e
Copter: Rate Pitch IMAX default to 1000
...
Spotted by Jonathan Challinger, thanks!
2014-10-07 21:06:43 +09:00
Andrew Tridgell
e0caee9500
Linux_HAL_Essentials: rebuilt rcinpru0 with 300 ring buffer entries
...
thanks to Sid for doing this
2014-10-07 14:57:35 +11:00
Andrew Tridgell
9b207d029d
HAL_Linux: change ring buffer to 300 entries
2014-10-07 14:57:34 +11:00
Andrew Tridgell
994b2597fd
Linux_HAL_Essentials: change ring buffer to 300 entries
...
this ensures full SBUS frames can be decoded
2014-10-07 14:57:34 +11:00
Andrew Tridgell
b1845ed00d
HAL_Linux: initial support for parallel SBUS and PPM-SUM decoding
2014-10-07 14:57:34 +11:00
Andrew Tridgell
42e9dc3c31
HAL_Linux: added SBUS decoder from PX4 project
...
thanks Lorenz!
2014-10-07 14:57:34 +11:00
Craig Elder
5b23f81e2b
Frame_params: Updating 3DR_X8-M_RTF.param
2014-10-06 16:07:49 -07:00
Craig Elder
5d7ec98d7a
Frame_params: Adding 3DR_X8-M_RTF.param
2014-10-06 15:44:35 -07:00
Andrew Tridgell
71d786187e
Plane: make auto takeoff independent of compass
...
this solves a problem of poor initial yaw due to poor compass offsets
causing a takeoff to not be in the direction the plane is pointing. A
summed gyro is used until the GPS speed is above 5m/s for 2 seconds,
then the GPS heading corrected by the summed gyro error is used for L1
based navigation for the rest of the takeoff
2014-10-07 07:17:46 +11:00
Andrew Tridgell
809b6cc855
AP_AHRS: added get_yaw_rate_earth()
...
used to estimate course correction on takeoff
2014-10-07 07:17:46 +11:00
Craig Elder
41ce8c2abd
Frame_params: 3DR_Iris+
...
Decreased ATC_RATE_RP_MAX to 18000
2014-10-06 12:17:52 -07:00
Craig Elder
be352e9471
AP_GPS: Removed CFG-DAT message from 3DR-Ublox-NEO7
...
CFG-DAT is generated by U-Center but no longer used by the receiver.
2014-10-06 11:21:42 -07:00
Randy Mackay
5e91d49736
Tracker: constrain manual pass through
2014-10-06 19:41:04 +09:00
Randy Mackay
4f5f253656
Tracker: send RADIO_IN msg to GCS
2014-10-06 19:41:02 +09:00
Randy Mackay
1b7ca684ee
Tracker: add read_radio
2014-10-06 19:41:01 +09:00
Randy Mackay
f4d45c9b6d
Tracker: limit yaw to YAW_RANGE
2014-10-06 19:40:59 +09:00
Randy Mackay
e7e0dd3509
Tracker: remove outdated comments
2014-10-06 19:40:58 +09:00
Randy Mackay
b6634bb416
Tracker: reorder servo functions
...
No functional change.
Flow runs from top to bottom with functions at top of file calling those
lower down.
2014-10-06 19:40:57 +09:00
Randy Mackay
a43a8ccfa0
Tracker: remove servo debug
2014-10-06 19:40:55 +09:00
Randy Mackay
704a720412
Tracker: move servo init to servos.pde
2014-10-06 19:40:54 +09:00
Randy Mackay
c69bfa2cb1
Tracker: limit pitch to PITCH_RANGE
...
Also set servo_limit flags for pitch
2014-10-06 19:40:53 +09:00
Randy Mackay
f2dab17230
Tracker: add YAW_RANGE and PITCH_RANGE params
...
These capture the yaw and pitch range of movement in degrees
2014-10-06 19:40:51 +09:00
Randy Mackay
1786c36457
Tracker: move nav_status lower in AntennaTracker.pde
...
No functional change
2014-10-06 19:40:50 +09:00
Randy Mackay
b9eaec8e97
Tracker: rename err variable to angle_err
...
No functional change
2014-10-06 19:40:48 +09:00
Randy Mackay
bf4ba9ffc4
Tracker: auto move servos only with valid vehicle position
2014-10-06 19:40:47 +09:00
Randy Mackay
0d1fefc23d
Tracker: vehicle state made global
2014-10-06 19:40:46 +09:00
Randy Mackay
2155951e63
Tracker: move startup delay to update_tracking call
...
This ensure the tracker does not move in any mode until after the
startup delay has passed
2014-10-06 19:40:44 +09:00
Randy Mackay
1135ef3610
Tracker: move servo control to servos.pde file
2014-10-06 19:40:43 +09:00
Randy Mackay
643a680fed
Tracker: move pos estimate to separate function
2014-10-06 19:40:41 +09:00
Randy Mackay
8e548ddabc
Tracker: move auto, manual and scan to separate files
2014-10-06 19:40:40 +09:00
Randy Mackay
7afd443f57
Tracker: move bearing and dist calcs to separate function
2014-10-06 19:40:39 +09:00