会议专题

Research on Quick Transfer Alignment for Aircraft Launched Moving Base

In order to evaluate the feasibility and performance of aircraft launched moving base, a quick transfer alignment algorithm and related simulation were established. The standardized eigenvalue method was analyzed and the dependence of transfer alignment performance on Kalman filter system model, system state error propagation and alignment duration were investigated. The simulation results showed that the entire duration of velocity alignment and attitude alignment was reduced to 7 seconds.

Aircraft Launched Moving Base Quick Transfer Alignment Eigenvalue Equation Kalman Filter

Dongzhu Feng Xin Wang

School of electronic engineering, Xidian University, Xi’an 710071, China College of Astronautics, Northwestern Polytechnical University, Xi’an 710072 China

国际会议

2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)

广西桂林

英文

3127-3130

2009-06-17(万方平台首次上网日期,不代表论文的发表时间)