Improving the high altitude performance of tail-controlled endoatmospheric missiles

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Zarchan, Paul ^a   Greenberg, Edwin ^a   Alpert, Joel ^a  

^a MIT LINCOLN LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; MISSILES; STRUCTURAL FRAMES;

AERODYNAMIC MISSILES; CLOSED FORM SOLUTIONS; FLIGHT CONTROL COMPUTER; HIGH ALTITUDE PERFORMANCE; NUMERICAL VALUES; OPTIMAL GUIDANCE; PROPORTIONAL NAVIGATION; RIGHT HALF PLANES;

NAVIGATION;

EID: 85089110260     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4770     Document Type: Conference Paper

References (5)

1. Zarchan, P., Tactical and Strategic Missile Guidance, Third Edition, Progress in Astronautics and Aeronautics, AIAA, Reston, VA 1998, pp. 507-523.
2. Willems, G., "Optimal Controllers For Homing Missiles," Report RE-TR-68-15, U.S. Army Missile Command, Redstone Arsenal, 1968.
3. Cottrell, R.G., "Optimal Intercept Guidance for Short-Range Tactical Missiles," AIAA Journal, Vol. 9, July 1971, pp. 1414-1415,
4. Bryson, A.E. and Ho, Y.C., Applied Optimal Control, Blaisdell, Waltham, MA, 1969.
5. Rusnak, I., and Meir, L., AIAA Journal of Guidance Control and Dynamics, Vol. 14, Number 5, pp. 1056-8, Sept.-Oct. 1991