Research on quick transfer alignment for aircraft launched moving base

Author

Feng, Dongzhu ; Wang, Xin

Author_Institution

Sch. of Electron. Eng., Xidian Univ., Xi´´an, China

fYear

2009

fDate

17-19 June 2009

Firstpage

3127

Lastpage

3130

Abstract

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.

Keywords

Kalman filters; aerospace engineering; aerospace simulation; aircraft; digital simulation; eigenvalues and eigenfunctions; Kalman filter system model; aircraft launched moving base; alignment duration; quick transfer alignment; standardized eigenvalue method; system state error propagation; transfer alignment performance; Aerospace electronics; Aerospace engineering; Aircraft propulsion; Educational institutions; Eigenvalues and eigenfunctions; Equations; Performance analysis; TV; Aircraft Launched Moving Base; Eigenvalue Equation; Kalman Filter; Quick Transfer Alignment;

fLanguage

English

Publisher

ieee

Conference_Titel

Control and Decision Conference, 2009. CCDC '09. Chinese

Conference_Location

Guilin

Print_ISBN

978-1-4244-2722-2

Electronic_ISBN

978-1-4244-2723-9

Type

conf

DOI

10.1109/CCDC.2009.5192935

Filename

5192935