Agile missile dynamics and control

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 3, 1998, Pages 441-449

  Wise, Kevin A ^a,b   Broy, David J ^a  

^a BOEING COMPANY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLIGHT DYNAMICS; LINEARIZATION; MATHEMATICAL MODELS; MISSILES;

AGILE MISSILE DYNAMICS;

NONLINEAR CONTROL SYSTEMS;

EID: 0032073562     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4256     Document Type: Article

References (8)

1. McRuer, D., Ashkenas, I., and Graham, D., Aircraft Dynamics and Automatic Control, Princeton Univ. Press, Princeton, NJ, 1973, pp. 203-262.
2. Blakelock, J. H., Automatic Control of Aircraft and Missiles, Wiley, New York, 1991, Chaps. 1-3.
3. Wassom, S. R., Faupell, L. C., and Perley, T., "Integrated Aerofin/TVC for Tactical Missiles," Journal of Propulsion and Power. Vol. 7, No. 3, 1991, pp. 374-381.
4. Wise, K. A., "Comparison of Six Robustness Tests Evaluating Missile Autopilot Robustness to Uncertain Aerodynamics," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 861-870.
5. Meriam, J. L., Dynamics, Wiley, New York, 1991, p. 244.
6. Hsu, C. S., and Robel, G., "Zeros and Transmission Zeros of Flight Control Systems," AIAA Guidance, Navigation, and Control Conference, AIAA, New York, 1987 (AIAA Paper 87-2237).
7. Douglas, R., Mackler, S., and Speyer, J., "Robust Hover Control for a Short Takeoff/Vertical Landing Aircraft," Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Washington, DC, 1990, pp. 150-163.
8. Wise, K. A., "Bank-to-Turn Missile Autopilot Design Using Loop Transfer Recovery," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, 1990. pp. 145-152.