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
Link To Document :
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