DocumentCode
1986077
Title
Design of new predictive guidance algorithm via fuzzy techniques
Author
Wang, Junbo ; Ren, Zhang ; Liang, Zixuan ; Xiong, Zihao
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2011
fDate
16-18 Sept. 2011
Firstpage
633
Lastpage
637
Abstract
New predictive guidance (NPG) algorithm is proposed and the fuzzy techniques are adopted to improve the real-time capability of the predictive guidance. The simplified kinematical and dynamical equations of model for the entry vehicle are established. The nominal bank angel profile is established beforehand to implement numerical prediction. The predictive errors are used as input of fuzzy logic controller which is designed for generation of correct commands. The fuzzy logic controller avoids massive iterations of conventional predictive guidance (CPG) algorithm and improves the real-time capability. Numerical simulations for the proposed algorithm under the condition of perturbations are presented to demonstrate the capability and effectiveness.
Keywords
fuzzy control; missile guidance; predictor-corrector methods; dynamical equations; fuzzy logic controller; fuzzy techniques; kinematical equations; new predictive guidance algorithm; numerical simulations; Algorithm design and analysis; Atmospheric modeling; Prediction algorithms; Real time systems; Trajectory; Vehicle dynamics; Vehicles; Entry vehicles; entry guidance; fuzzy logic controller; predictive guidance;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical and Control Engineering (ICECE), 2011 International Conference on
Conference_Location
Yichang
Print_ISBN
978-1-4244-8162-0
Type
conf
DOI
10.1109/ICECENG.2011.6057648
Filename
6057648
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