Advanced guidance laws for acceleration constrained missile, randomly maneuvering target and noisy measurements

1st IEEE Regional Conference on Aerospace Control Systems, AEROCS 1993 - Proceedings

Volumn , Issue , 1993, Pages 594-598

  Rusnak, I ^a  

^a DREXEL UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; CONTROL SYSTEMS;

ARBITRARY ORDER; CLOSED-FORM FORMULAE; DETERMINISTIC SYSTEMS; INITIAL CONDITIONS; MANEUVERING TARGETS; NOISY MEASUREMENTS; OPTIMAL GUIDANCE LAW; TIME INVARIANTS;

GUIDED MISSILES;

EID: 85006901940     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AEROCS.1993.721003     Document Type: Conference Paper

References (8)

1. Bryson, A. E., Jr., Ho, Y. C.:"Applied Optimal Control", Blaisdell Publishing Company, Waltham, Massachusets, 1969.
2. Rusnak, I., Meir, L. : "Optimal Guidance for High Order and Acceleration Constrained Missile", Journal of Guidance, Control and Dynamics, Vol. 14, No. 3, May-June 1991, pp. 589-596.
3. Rusnak, I., Meir, L. :"Optimal Guidance for Acceleration Constrained Missile and Maneuvering Target", IEEE Trans, on AES, Vol. 26, AES-26, No. 4, July 1990.
4. Gelb, A., Vander Velde, W.E.:"Multiple-Input Describing Functions and Nonlinear System Design, " McGraw-Hill, 1968.
5. Rusnak, I., Meir, L. :"Modern Guidance Law for High Order Autopilot", Journal of Guidance, Control and Dynamics, Vol. 14, No. 5, September-October 1991.
6. Rusnak, I.: "Optimal Guidance for High Order Randomly Maneuvering Target and High Order Missile", ICCON-89, 3-6 April 1989, Jerusalem, Israel.
7. Rusnak, I. :"Optimal Control of Input Constrained Linear Systems, " 35-th Midwest Symposium on Circuits and Systems, August 9-12, 1992, Washington, D.C., 1992.
8. Fitzgerald, R.J., Zarchan, P.:"Shaping Filters for Randomly Initiated Targets Maneuvers", AIAA Paper 78-1304, Palo Alto, Calif., 1978.