DocumentCode
1794901
Title
A rapid endgame performance analysis method for exoatmosphere interceptor based on CADET
Author
TaoTao Zhang ; CongYing Li ; Zhiyong Yang
Author_Institution
7th Dept., Naval Astronaut. & Aeronaut. Univ., Yantai, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
558
Lastpage
563
Abstract
The relative equations between interceptor and target are conducted in rotation coordinate of Line of Sight. An error propagate model of LOS rate is established which is based on CADET (Covariance Analysis Describing Function Technique). This model takes several factors into consideration, such as estimate error of LOS rate, acceleration saturation of interceptor, sampling rate. A set of analytical solution is acquired. The uncertainty of Zero Effort Miss distance can be got conveniently according to the variety of LOS rotate rate. Finally, a contrast simulation with Mont-Carlo is taken to demonstrate the preciseness and efficiency of the method proposed in this paper.
Keywords
Monte Carlo methods; aerospace instrumentation; covariance analysis; CADET; LOS rate; Monte Carlo method; covariance analysis describing function technique; error propagate model; exoatmosphere interceptor; rapid endgame performance analysis method; zero effort miss distance uncertainty; Acceleration; Analytical models; Covariance matrices; Equations; Mathematical model; Uncertainty; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007283
Filename
7007283
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