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Tree: 4c96ec26e5

AP_Periph-1.3

Copter-4.2

Copter-4.2-BW

apm_2208

apm_2208-rover

apm_2208-rover-debug

c421

copter407

gps-1.3.1

main

master

master_rangefinder

mission-4.1.18

periph-1.3.1

release-4.2.3

rover_4.3

zr-sdk-4.3.1

zr-v5.0

zr-v5.1

zr/Rover-4.3

zr/main-4.3

zr_rover4.2

数字绿土/zr-v5.0

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ardupilot/libraries/AP_NavEKF

History

Andrew Tridgell 411a96b4b3 AP_NavEKF: take at most 30s to accept DCM attitude ... velocity noise on the GPS can cause DCM to take a long time to converge. If it takes longer than 30s then allow EKF to start		10 years ago
..
Models	AP_NavEKF: Add Matlab derivations and simulations behind small EKF	10 years ago
AP_NavEKF.cpp	AP_NavEKF: take at most 30s to accept DCM attitude	10 years ago
AP_NavEKF.h	AP_NavEKF: Enforce alignment of realigned earth mag field with declination	10 years ago
AP_Nav_Common.h	AP_NavEKF: added using_gps status bit	10 years ago
AP_SmallEKF.cpp	AP_NavEKF: float to double promotion via tan instead of tanf	10 years ago
AP_SmallEKF.h	AP_SmallEKF: add function to report if the EKF is stable	10 years ago