Title :
The input estimator design and application in estimating atmospheric disturbances for aircraft systems
Author_Institution :
Dept. of Aircraft Eng., Army Acad., Jungli, Taiwan
Abstract :
In this work, the Input-Estimation IE algorithm based on Kalman filter F is proposed to estimate the atmospheric disturbance. It can hold a high disturbance estimating performance when system variation is unknown and under the disturbances. The input estimation algorithm is an on-line inverse estimation method that based on the F and least square method, which estimate the system disturbance without extra sensors. The estimation performance of the proposed estimator is also studied in estimating the atmospheric disturbance for the aircraft system. The simulation results shown that the proposed estimator can be a good disturbance estimator for aircraft system in estimating the atmospheric disturbance.
Keywords :
Kalman filters; aircraft instrumentation; atmospheric pressure; estimation theory; pressure measurement; Kalman filter; aircraft systems; atmospheric disturbance; atmospheric disturbances estimation; input estimation IE algorithm; least square method; online inverse estimation method; system disturbance estimation; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft propulsion; Atmosphere; Atmospheric measurements; Control systems; Military aircraft; Noise measurement; Time measurement;
Conference_Titel :
Computer Communication Control and Automation (3CA), 2010 International Symposium on
Conference_Location :
Tainan
Print_ISBN :
978-1-4244-5565-2
DOI :
10.1109/3CA.2010.5533592