Source: modules/attitude_estimator_q
Attitude and position estimator using an Extended Kalman Filter. It is used for Multirotors and Fixed-Wing.
AttitudeEstimatorQ <command> [arguments...]
wind_estimator <command> [arguments...]
Commands:
start
stop
status 打印状态信息
The documentation can be found on the tuning_the_ecl_ekf page.
This module provides a single airspeed_validated topic, containing indicated (IAS), calibrated (CAS), true airspeed (TAS) and the information if the estimation currently is invalid and if based sensor readings or on groundspeed minus windspeed. Supporting the input of multiple "raw" airspeed inputs, this module automatically switches to a valid sensor in case of failure detection. For failure detection as well as for the estimation of a scale factor from IAS to CAS, it runs several wind estimators and also publishes those.
airspeed_estimator <command> [arguments...]
wind_estimator <command> [arguments...]
Commands:
start
stop
status 打印状态信息
源码:modules/ekf2
基于扩展卡尔曼滤波器的姿态和位置估计器。 该模块同时应用于多旋翼和固定翼飞机。
Source: modules/wind_estimator
This module runs a combined wind and airspeed scale factor estimator. If provided the vehicle NED speed and attitude it can estimate the horizontal wind components based on a zero sideslip assumption. This makes the estimator only suitable for fixed wing vehicles. If provided an airspeed measurement this module also estimates an airspeed scale factor based on the following model: measured_airspeed = scale_factor * real_airspeed.
ekf2 <command> [arguments...]
ekf2 <command> [arguments...]
Commands:
start
[-r] 启用 replay 模式
stop
status 打印状态信息
源码:modules/local_position_estimator
基于扩展卡尔曼滤波器的姿态和位置估计器。
local_position_estimator <command> [arguments...]
Commands:
start
stop
status 打印状态信息
wind_estimator <command> [arguments...]
Commands:
start
stop
status 打印状态信息
Source: modules/mc_hover_thrust_estimator
mc_hover_thrust_estimator <command> [arguments...]
wind_estimator <command> [arguments...]
Commands:
start
stop
status 打印状态信息