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
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