Title :
Angular acceleration estimator for a flight motion simulator: Design and performance comparison
Author :
Ma, Jie ; Yao, Yu
Author_Institution :
Harbin Inst. of Technol., Harbin, China
Abstract :
Angular acceleration feedback will help improve dynamic transparency and reduce non-linear behavior of flight motion simulator axes motions. FIR and Kalman angular acceleration estimator design method are investigated in this paper. A detailed performance comparison is proposed and the results indicate the angular acceleration estimators present an effective routine to produce the high fidelity flight motion simulator.
Keywords :
FIR filters; Kalman filters; acceleration control; aerospace control; aerospace simulation; angular velocity control; angular velocity measurement; feedback; motion control; FIR filter; Kalman filter; angular acceleration estimator; angular acceleration feedback; axes motion; dynamic transparency; flight motion simulator; nonlinear behavior; Acceleration; Accelerometers; Aerospace simulation; Computational modeling; Control system synthesis; Finite impulse response filter; Kalman filters; Motion control; Motion estimation; Optical sensors;
Conference_Titel :
Control and Automation, 2009. MED '09. 17th Mediterranean Conference on
Conference_Location :
Thessaloniki
Print_ISBN :
978-1-4244-4684-1
Electronic_ISBN :
978-1-4244-4685-8
DOI :
10.1109/MED.2009.5164609
