DocumentCode :
1803667
Title :
An advanced estimation design for high speed reentry targets
Author :
Chen, Yung-Yue ; Lin, Chun-Liang ; Huang, Chun-Wei ; Lin, Yu-Pin
Author_Institution :
Dept. of Electr. Eng., Nat. Yunlin Univ. of Sci. & Technol., Douliou, Taiwan
fYear :
2011
fDate :
15-18 May 2011
Firstpage :
470
Lastpage :
475
Abstract :
Trajectory estimation design of tactical ballistic missiles (TBM) is an important issue to build up an anti-missile system and attracts a lot of attentions in it. Unfortunately, the relative trajectory estimation technologies are still secrets of "specific countries" and of course, cannot be easily obtained. Based on this reason, in this research, an advanced trajectory estimation design is investigated with combined the input estimation and extended Kalman filter. In this proposed method, estimation abilities extend from high speed reentry target\´s position and velocity to uncertain maneuverable accelerations and ballistic coefficient, i.e., more information of the targets can be offered by this method, besides, the acceptable trajectory estimation performance are shown from scenarios with different testing conditions.
Keywords :
Kalman filters; ballistics; design; estimation theory; missile control; position control; advanced estimation design; advanced trajectory estimation design; ballistic coefficient; extended Kalman filter; high speed reentry target; relative trajectory estimation technologies; tactical ballistic missiles; trajectory estimation design; uncertain maneuverable accelerations; Estimation; Kalman filters; Radar tracking; Target tracking; Trajectory; Zirconium; Ballistic Missile; Extended Kalman Filter; Input Estimation; Trajectory Estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ASCC), 2011 8th Asian
Conference_Location :
Kaohsiung
Print_ISBN :
978-1-61284-487-9
Electronic_ISBN :
978-89-956056-4-6
Type :
conf
Filename :
5899117
Link To Document :
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