DocumentCode
1794975
Title
Ballistic missile trajectory prediction and the solution algorithms for impact point prediction
Author
Xu Zhang ; Hu-Min Lei ; Jiong Li ; Da-Yuan Zhang
Author_Institution
Navig. & Control Lab., Air Force Eng. Univ., Xi´an, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
879
Lastpage
883
Abstract
In order to improve the guidance precision of the ballistic missile interception, the target´s trajectory prediction and the impact point prediction solution algorithm for interceptor´s mid-course guidance are studied. Firstly, in allusion to the drawbacks of current ballistic missile´s trajectory predication, the high precision ballistic missile prediction algorithms based on predictor-corrector method considering the radar´s measurement noise are designed on the premise of ballistic missile tracking. Then, in allusion to the drawbacks of dead circulation, heavy computation, and engineering unavailability in current impact point prediction solving, the basic strategy of impact point prediction guidance is studied, and the iterative solution algorithm of forecasting impact point based on time series is designed with common applicability, less computation and engineering availability, and then the computing circuit is proposed. Simulations results show that the proposed algorithms of ballistic trajectory prediction and impact point prediction solution have better precision and availability, which could offer some theoretical meaning and some references for engineering application.
Keywords
iterative methods; missile guidance; time series; trajectory control; ballistic missile interception; ballistic missile tracking; ballistic missile trajectory prediction; impact point prediction; interceptor mid-course guidance; iterative solution algorithm; predictor-corrector method; radar measurement noise; time series; Equations; Forecasting; Missiles; Prediction algorithms; Predictive models; Target tracking; Trajectory;
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.2014.7007325
Filename
7007325
Link To Document