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14,544 Commits 71 Branches 509 Tags 747 MiB
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14544 Commits

Author SHA1 Message Date
Randy Mackay 4521d8169b Rover: BATT param's underscore moved to library 2014-12-31 15:22:56 +09:00
Randy Mackay 6bec527aa3 Plane: BATT param's underscore moved to library 2014-12-31 15:22:56 +09:00
Randy Mackay 7d18744094 Plane: use battery.voltage2 method for logging 2014-12-31 15:22:55 +09:00
Randy Mackay 5cdb8a4c2a Plane: use battery.has_current 2014-12-31 15:22:54 +09:00
Randy Mackay fe8730497a Rover: use battery.has_current 2014-12-31 15:22:53 +09:00
Randy Mackay b4b062e9ef PX4: start batt_smbus 2014-12-31 15:22:52 +09:00
Randy Mackay 70dcc724ac PX4: add batt_smbus module to build 2014-12-31 15:22:52 +09:00
Randy Mackay 909d525206 BattMon: fix example sketch compile error 2014-12-31 15:22:51 +09:00
Randy Mackay f1f71ef605 Copter: cli uses has_current method 2014-12-31 15:22:50 +09:00
Randy Mackay 3ccc61c163 Copter: use battery.has_current method 2014-12-31 15:22:49 +09:00
Randy Mackay cf36fd55bd GCS_MAVlink: correct sending of 2nd battery's voltage 2014-12-31 15:22:49 +09:00
Randy Mackay d6b4bfd97f Copter: move underscore in BATT_ parameters 2014-12-31 15:22:48 +09:00
Randy Mackay 76a28a962c BattMon: remove #defines for monitor type 2014-12-31 15:22:47 +09:00
Randy Mackay f077ecd338 BattMon_PX4: class to read from PX4Firmware via orb 2014-12-31 15:22:46 +09:00
Randy Mackay 3f35dc54fe BattMon_I2C: smart battery class for APM 2014-12-31 15:22:45 +09:00
Randy Mackay 314db1403d BattMon_SMBus: smart battery monitor driver 2014-12-31 15:22:45 +09:00
Randy Mackay 4d7df9ed26 BattMon_Analog: move analog features to new class 2014-12-31 15:22:44 +09:00
Randy Mackay 39dbf05c8f BattMon_Backend: create backend class 2014-12-31 15:22:43 +09:00
Randy Mackay eec66d8451 BattMon: parent class becomes frontend class 2014-12-31 15:22:42 +09:00
Randy Mackay 9be53502df Plane: remove logging dependecy on optflow 2014-12-31 15:22:41 +09:00
Randy Mackay d46ceac1f8 Git: ignore autotest.lck and index.html 2014-12-31 14:05:14 +09:00
Randy Mackay c36253b9b2 AC_PosControl: add comments 
No functional change
 2014-12-31 14:03:22 +09:00
Jonathan Challinger 6eab698e85 AC_WPNav: remove various timing hacks 2014-12-31 14:03:20 +09:00
Jonathan Challinger 557d339cf1 AC_PosControl: remove various unnecessary timing hacks 2014-12-31 14:03:18 +09:00
Jonathan Challinger 5438d38df5 AC_WPNav: provide reset_I to init_xy_controller 2014-12-31 14:03:16 +09:00
Jonathan Challinger d6e455417f AC_PosControl: change keep_xy_I_terms to a parameter of init_xy_controller 2014-12-31 14:03:13 +09:00
Randy Mackay 8960766900 Rover: remove logging dependency on optflow 2014-12-31 13:16:18 +09:00
Randy Mackay 2e7435df52 Copter: remove unused OF_LOITER pid defines 2014-12-31 13:16:18 +09:00
Randy Mackay 3e34e7ed7e Copter: remove logging dependency on optflow 2014-12-31 13:16:17 +09:00
priseborough b016bae445 AP_NavEKF: Clean up reset of constant velocity mode 
Move velocity store out of optical flow to velocity and position fusion control as it is a velocity fusion function.
Always clear the previous mode status
 2014-12-31 13:16:16 +09:00
priseborough 3d207c316a AP_NavEKF: Change names for position and velocity hold modes 
Name change done to avoid confusion with flight modes. modes are now referred to as constant position and constant velocity mode.
 2014-12-31 13:16:15 +09:00
priseborough b650ee51a9 AP_NavEKF: Consolidate arming checks 2014-12-31 13:16:15 +09:00
priseborough 48cae0df15 AP_NavEKF: Fall back to attitude and hgt estimation for copter if GPS lost 2014-12-31 13:16:14 +09:00
priseborough b21f9daa90 AP_NavEKF: Update solution status reporting 
This patch makes the reporting of an absolute position solution less abbiguaous and ensures that relative position is always true if absolute position is true
 2014-12-31 13:16:13 +09:00
priseborough ee75f26edb Rover: Don't log EKF optical flow data if not required 2014-12-31 13:16:12 +09:00
priseborough 695f12bec0 Copter: Don't log EKF optical flow data if not required 2014-12-31 13:16:12 +09:00
priseborough 195cdb6fd6 Plane: Don't log EKF optical flow data if not required 2014-12-31 13:16:11 +09:00
priseborough 9c8406998b Replay: Don't log EKF optical flow data if not required 2014-12-31 13:16:10 +09:00
priseborough b99b3c7b9d DataFlash: Don't log EKF optical flow data if not required 2014-12-31 13:16:09 +09:00
priseborough b6d300db19 AP_NavEKF: clean up determination of GPS availability 2014-12-31 13:14:22 +09:00
priseborough 40b02fc19a AP_NavEKF: Ensure filter doesn't try to use GPS after initialisation 2014-12-31 13:14:20 +09:00
priseborough bab1a69f1c AP_NavEKF: make position and velocity resets consistent with GPS usage 2014-12-31 13:14:18 +09:00
priseborough 0dc2356175 AP_NavEKF: Ensure initialisation methods read required sensor data 2014-12-31 13:14:16 +09:00
priseborough 5d1de79f08 AP_NavEKF: Modify initial values to make startup behaviour more consistent 2014-12-31 13:14:14 +09:00
priseborough a63af34d8f AP_NavEKF: Allow 10 seconds for the filter to settle after initialisation 
Filter is declared unhealthy and will not arm for first 10 seconds after initialisation
 2014-12-31 13:14:12 +09:00
priseborough 0a5de21dc7 AP_NavEKF: Fix bug in reporting of solution status 
Because synthetic  position measurements at 0,0 are fused during position hold mode, a position timeout cannot be used as the only means of detecting position solution status.
 2014-12-31 13:14:09 +09:00
priseborough 92c3026072 AP_NavEKF: Link process noise to arm status, not pos hold mode 2014-12-31 13:14:07 +09:00
priseborough a535b73a6d AP_NavEKF: Initialise timeout status to true 
This status will be cleared when data arrives and is fused successfully
 2014-12-31 13:14:04 +09:00
priseborough 363c1e393d AP_NavEKF: Latch use of position hold mode for duration of flight 
Required to prevent acquisition of GPS mid flight causing unwanted change in position and velocity
A distinction has been mad between the arm and disarm transition and the decision to use position hold mode (formerly static mode)
 2014-12-31 13:14:02 +09:00
priseborough a0a6c0362f AP_NavEKF: Relax timeout check applied to optical flow data 
200 msec was too short and could lead to false positives. 5000 msec is the largest time we can go free inertial.
 2014-12-31 13:14:00 +09:00