Missile guidance algorithm design using inverse kinematics and fuzzy logic

Fuzzy Sets and Systems

Volumn 79, Issue 3, 1996, Pages 287-295

  Leng, Gerard ^a  

^a NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

Aerospace engineering; Guidance algorithm design; Inverse kinematics

Indexed keywords

EID: 0012578512     PISSN: 01650114     EISSN: None     Source Type: Journal    
DOI: 10.1016/0165-0114(95)00172-7     Document Type: Article

References (10)

1. C. Baker, Fuzzy logic control in flight control systems, in: M. Jamshidi, N. Vadiee and T.J. Ross, Eds., Fuzzy Logic and Control, Software and Hardware Applications (Prentice-Hall, New Jersey, 1993).
2. A. Bryson and Y.C. Ho, Applied Optimal Control (Hemisphere, New York, 1975).
3. S. Chiu et al., Fuzzy logic for control of roll and moment for a flexible wing aircraft, IEEE Control Systems Mag. (June 1991) 42-48.
4. C.C. Lee, Fuzzy logic in control systems: Fuzzy logic controller - Part I, IEEE Trans Systems, Man and Cybernetics 20(2) (1990) 404-418.
5. C.C. Lee, Fuzzy logic in control systems: Fuzzy logic controller - Part II, IEEE Trans. Systems, Man and Cybernetics 20(2) (1990) 419-435.
6. G. Leng, Missile guidance using fuzzy logic and inverse kinematics, in: Proc. 5th MINDEF-NUS Defence R&D Seminar (Ministry of Defence, Singapore, (1993), 1-7.
7. A. Locke, Guidance (van Nostrand, New York, 1955).
8. W. Pedrycz, Fuzzy Control and Fuzzy Systems (Wiley, New York, 1989).
9. S. Suzuki and T. Yoshizawa, Multiobjective trajectory optimization by goal programming with fuzzy decisions, J. Guidance, Control and Dynamics 17(2) (1994), 297-303.
10. P. Zachran, Tactical and Strategic Missile Guidance, AIAA Progress in Astronautics and Aeronautics, Vol. 124, Washington D.C., 1990.