Optimal guidance laws with uncertain time-of-flight

IEEE Transactions on Aerospace and Electronic Systems

Volumn 36, Issue 2, 2000, Pages 721-725

  Rusnak, Ilan ^a  

^a RAFAEL   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; DISCRETE TIME CONTROL SYSTEMS; LINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS; PROBABILITY DENSITY FUNCTION; UNCERTAIN SYSTEMS;

TIME-OF-FLIGHT;

FLIGHT DYNAMICS;

EID: 0033746930     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.845272     Document Type: Article

References (8)

1. Bryson, A. E., and Ho, Y. C. (1975) Applied Optimal Control. New York: Hemisphere, 1975, ch. 5.
2. Nesline, F. W., and Zarchan, P. (1981) A new look at classical versus modern homing guidance. Journal of Guidance, Control, and Dynamics, 4, 1 (Jan.-Feb. 1981), 78-85.
3. Ben-Asher, J., and Yaesh, I. (1998) Advances in Missile Guidance Theory, vol. 180 (Progress in Astronautics and Aeronautics). Washington, DC: AIAA Inc., 1998, ch. 5.
4. Ben-Asher, J., and Yaesh, I. (1997) Optimal guidance with reduced sensitivity to time-to-go estimation errors. Journal of Guidance and Control, and Dynamics, 20, 1 (1997), 158-163.
5. Zarchan, P. (1997) Tactical and Strategic Missile Guidance, vol. 176 (3rd ed.) (Progress in Astronautics and Aeronautics). Washington, DC: AIAA Inc., 1997.
6. Rusnak, I., and Levi, M. (1991) Optimal guidance for high-order and acceleration constrained missile. Journal of Guidance and Control, and Dynamics, 14, 3 (1991), 589-596.
7. Riggs, T. (1979) Linear optimal guidance for short range air-to-air missiles. In Proceedings of National Aerospace and Electronics Conference, 1979, 757-764.
8. Sivan, R. (1966) The optimal control of linear systems with unknown final time. IEEE Transactions on Automatic Control, AC-11, 4 (1966), 529-530.