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FUZZY TERMINAL ATTITUDE GUIDANCE CONTROLLER WITH ANGLE ONLY MEASUREMENTS
P.N. Pathirana and F.A. Faruqi
References
[1] A.V. Savkin, P.N. Pathirana, & F.A. Faruqui, Precision missileguidance with H∞ vs LQR control, Proc. IEEE Conf. onDecision and Control, 2, Florida, USA, 4–7 December 2001,1535–1540.
[2] A.V. Savkin, & P.N. Pathirana, Interceptor end-game trajectory shaping for precision-guided weapons, Report for DefenseScience Technology Organization, Adelaide, Australia, 2000.
[3] A.V. Savkin, P.N. Pathirana, & F.A. Faruqi, The problem ofprecision missile guidance: LQR and H∞ control framework,IEEE Trans. on Aerospace and Electronic Systems, 39(3),2003, 901–910.
doi:10.1109/TAES.2003.1238744
[4] P.N. Pathirana, A.V. Savkin, & F.A. Faruqi, Missile guidancewith angle only measurements, Proc. Conf. on InformationDecision and Control, Adelaide, Australia, 11–13 February2002, 271–276.
[5] P.N. Pathirana, A.V. Savkin, & S. Jha, Location estimationand trajectory prediction for cellular networks with mobilebase stations, IEEE Trans. on Vehicle Technology, 53(6), 2004,1903–1913.
doi:10.1109/TVT.2004.836967
[6] C.M. Lin & Y.J. Mon, Fuzzy-logic-based guidance law designfor missile systems, Proc. Int. Conf. on Control Applications,1, Kohala Coast-Island of Hawaii, USA, 22–27 August 1999,421–426.58
[7] T.W. Vanek, Fuzzy guidance controller for an autonomousboat, IEEE Control Systems, 17(2), April 1997, 43–51.
doi:10.1109/37.581294
[8] T. Hessburg & M. Tomizuka, Fuzzy logic control for lateralvehicle guidance, IEEE Control Systems, 14(4), August 1994,55–63.
doi:10.1109/37.295971
[9] P. Zarchan, Proportional navigation and weaving targets,Journal of Guidance and Control, 18(5), 1995, 969–975.
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Abstract
DOI:
10.2316/Journal.201.2007.1.201-1636
From Journal
(201) Mechatronic Systems and Control (formerly Control and Intelligent Systems) - 2007
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