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Author SHA1 Message Date
Andrew Tridgell
983ac9cbf4 GCS_MAVLink: merge in latest upstream XML changes 2014-05-15 21:14:21 +10:00
Andrew Tridgell
1a05c27bbb AP_AHRS: added healthy() function 
this will be used to report when the AHRS subsystem becomes unhealthy
 2014-05-15 21:14:21 +10:00
Andrew Tridgell
086142580a AP_InertialSensor: added VibTest sketch 
logs all accel data at high rate to SD card
 2014-05-15 21:14:21 +10:00
Andrew Tridgell
47926dc6ea Replay: fixed for changes to AP_Compass HIL API 2014-05-15 21:14:21 +10:00
Jonathan Challinger
e883b889b6 SITL: Add compassmot interference 2014-05-15 21:14:20 +10:00
Randy Mackay
409a593c1a Plane: prepended APM to RSSI_PIN's @Values 
This makes it consistent with rover and copter and clarifies where the
pin is on the Pixhawk
 2014-05-15 17:13:48 +09:00
Randy Mackay
d7e015db89 Rover: add Pixhawk pin to RSSI_PIN's @Value 
Also prepended APM2 to existing values.  Added A2 to list to be
consistent with plane and copter
 2014-05-15 17:13:46 +09:00
Randy Mackay
9f81e286d1 Copter: add Pixhawk pin to RSSI_PIN's @Value 
Also prepend APM2 to existing definitions
 2014-05-15 17:13:43 +09:00
Randy Mackay
8b92ff4695 Rover: remove unused RELAY_PIN definition 
This is now part of the AP_Relay library
 2014-05-15 17:13:40 +09:00
Randy Mackay
4ebde25a26 AP_Relay: add -1:Disabled to list of param values 2014-05-15 17:13:37 +09:00
Randy Mackay
f7a9ee24ef Copter: minor comment update 2014-05-15 16:21:35 +09:00
Randy Mackay
715e9c0474 Copter: reset mission when disarming 2014-05-15 16:21:32 +09:00
Randy Mackay
7d4c74c28e Copter: when leaving AUTO only stop mission if running 
This resolves an issue in which the mission would not automatically
start from the beginning if it had previously been run to completion
 2014-05-15 16:21:30 +09:00
Randy Mackay
5d20594fa4 AC_WPNav: bug fix for loiter and waypoint update rate 
Thanks to EmileC for spotting this
 2014-05-12 20:13:46 +09:00
Andrew Tridgell
48919b6253 Rover: use EKF velocity for high rate ground_speed updates 
this may give smoother throttle response when the EKF is enabled
 2014-05-11 21:39:06 +10:00
Andrew Tridgell
85ebe81ed3 AP_NavEKF: fixed logic for divergence test 
Pair-Programmed-With: Paul Riseborough <p_riseborough@live.com.au>
 2014-05-11 18:00:38 +10:00
priseborough
40dc0e56fe AP_NavEKF: Add protection for badly conditioned innovation variances 2014-05-11 18:00:38 +10:00
priseborough
925c5751bd AP_NavEKF: Add ability to inhibit in-flight mag cal and clean up moding 
This will enable in-flight magnetometer calibration to be inhibited unconditionally,
This is required for long balloon carriage flights where ground speed can be high
enough to put it into in-air state, but with very poor observability of magnetic field
states causing bad state estimates and heading offsets to develop over time.

The covariance matrix no longer has rows and columns artificially zeroed when in static
mode. Instead booleans indicating whether wind or magentic field state estimation is
active are used to:

a) Set the process noise on these states to zero to stop their variances from increasing
unchecked when not being updated, and
b) Turn off updates for these states when measurement fusion is being performed.

This reduces the likelihood of a badly conditioned covariance matrix forming
during static mode operation.

A filter divergence check has also been added that will declare the filter unhealthy if
position, velocity and magnetic field observations are all failing their innovation
consistency checks. This unhealthy status will persist for 10 seconds after the
condition clears.

AP_NavEKF: Remove unnecessary zeroing of wind covariances
 2014-05-11 18:00:38 +10:00
priseborough
3026ccee13 AP_NavEKF: Use baro data during launch transients whilst in static mode 
Baro data can be used as it will still be valid during the launch and
is not a synthesised measurement.
 2014-05-11 18:00:38 +10:00
Randy Mackay
a38e00c048 Copter: remove unused HIGH, LOW definitions 
Minor commit to kick off the auto build so AC3.2-rc1 will go out
 2014-05-09 16:35:21 +09:00
Randy Mackay
3f329d0857 Copter: version to AC3.2-rc1 2014-05-09 13:48:47 +09:00
Randy Mackay
e75d6a2da6 Copter: remove meaningless check from motor_test 2014-05-09 13:48:44 +09:00
Randy Mackay
0c7a3f1ec5 Copter: remove unused Log_Write_GPS function 2014-05-09 13:48:41 +09:00
Randy Mackay
b4dcad725c Copter: remove unused servo_write function 2014-05-09 13:48:38 +09:00
Randy Mackay
1e8b99ad17 Copter: update release notes for AC3.2-rc1 2014-05-09 13:48:35 +09:00
Randy Mackay
05f5164dfa Mission: rename AUTORESET to RESTART 2014-05-09 11:31:37 +09:00
Andrew Tridgell
cc1b75ad29 autotest: restore timeout in log download 
this removes the debug code now that the issue has been found (it was
an old version of pymavlink causing the problem)
 2014-05-09 09:50:22 +10:00
Andrew Chapman
3f0a52cb53 Copter: ch7/8 switch for auto pause/continue 
- added new mode for CH7/CH8 (#24, auto mission reset)
- changed mission.start() to mission.start_or_resume() in auto_init()
 2014-05-08 23:09:42 +09:00
Andrew Chapman
8640e11728 Copter: bug fix rally point landing target 
was drifting toward home by some distance as (0,0,0) was hard-coded in
control_rtl.pde. Fixed, tested in SITL
 2014-05-08 23:09:40 +09:00
Hug0
6b0d5f9770 AP_InertialNav: fix pos error degradation rate 
degrate position_error to 10% over 2 seconds (assumes 5hz update rate)
must be *0.7943 instead of 0.7934
 2014-05-08 23:09:39 +09:00
Andrew Tridgell
73dc32108f autotest: try to debug log download timeouts 2014-05-08 17:38:49 +10:00
Randy Mackay
badc127c34 AC_WPNav: fix example sketch 2014-05-08 16:25:13 +09:00
Randy Mackay
9b6a4e0fc7 AC_Sprayer: fix example sketch 2014-05-08 16:25:11 +09:00
lthall
9ab9eaec25 AC_WPNav: Loiter jerk default to 10m/s/s/s 
Pair programmed with Randy
 2014-05-08 16:16:05 +09:00
Randy Mackay
197d83e32a Copter: bug fix to sport roll pitch control 2014-05-08 16:16:02 +09:00
Randy Mackay
0af9d502d9 Copter: set pos controller speeds before circle init 
This ensures stopping point is calculated correctly
 2014-05-08 16:15:59 +09:00
Randy Mackay
1cb297580f Copter: reduce Circle init twitch by using stopping point 2014-05-08 16:15:57 +09:00
Randy Mackay
3cc5b9446f Copter: AUTO and Guided call wp_and_spline_init 2014-05-08 16:15:55 +09:00
Randy Mackay
11918869a5 Copter: RTL calls wp_and_spline_init 2014-05-08 16:15:52 +09:00
Randy Mackay
091ff91a70 WPNav: add wp_and_spline_init to set speeds an init pos controller 2014-05-08 16:15:50 +09:00
Randy Mackay
c13db680b7 AC_PosControl: remove reset_I_xy 
lean_angles_to_accel is now used to load the position rate I terms based
on vehicle's initial roll and pitch angle
 2014-05-08 16:15:48 +09:00
Randy Mackay
cd8b1f278c AC_PosControl: remove unused _cos_yaw variable 
Also removed _sin_yaw, _cos_pitch, _step saving a total of 17bytes of
RAM
Also made get_speed_up, get_speed_down, lean_angles_to_accel functions
const
 2014-05-08 16:15:46 +09:00
Randy Mackay
48ec0caf75 AC_WPNav: run navigation at 10hz in SITL 2014-05-08 16:15:44 +09:00
Randy Mackay
0819e05896 AC_PosControl: lean_angles_to_accel added for smooth initialisation 
init_xy_controller also added to capture initialisation all in one place
 2014-05-08 16:15:41 +09:00
lthall
b38c484874 AC_WPNav: add LOIT_JERK parameter 
Limit accel output from loiter controller.
Call new pos_control.init_xy_controller when loiter starts
Remove sudden stop when pilot requested acceleration is zero

Pair programmed with Randy
 2014-05-08 16:15:38 +09:00
Randy Mackay
71fae1e6f2 AC_AttControl: lean_angle_max accessor fn const 2014-05-08 16:15:36 +09:00
Randy Mackay
ff1a58e078 Copter: increase LOITER_RATE_IMAX to 1000 
This allows us to load up the I term with the vehicle's current
acceleration during mode transitions

pair programmed with Randy
 2014-05-08 16:15:34 +09:00
Randy Mackay
fb2be07b44 Copter: update AC_WPNav instantiation 2014-05-08 16:15:29 +09:00
Randy Mackay
fd9f8f571f AC_WPNav: replace inav, ahrs pointers with references 2014-05-08 16:15:26 +09:00
lthall
21c93e48ab AC_PosControl: include vel error when get_stopping_point_z 
Pair programmed with Randy
 2014-05-08 16:15:24 +09:00