Assessment of air-to-air missile guidance and control technology
- 1 October 1989
- journal article
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Control Systems Magazine
- Vol. 9 (6) , 27-34
- https://doi.org/10.1109/37.41440
Abstract
Current air-to-air missile guidance and control technology is assessed. Areas explored include target state estimation, advanced guidance laws, and bank-to-turn autopilots. The assumptions, benefits, and limitations of recent applications of nonlinear filtering, adaptive filtering, modern control, adaptive control, dual control, differential game theory, and modern control design techniques to the air-to-air missile problem are discussed.Keywords
This publication has 47 references indexed in Scilit:
- Assumed density filter with application to homing missile guidanceJournal of Guidance, Control, and Dynamics, 1989
- Reduced-order pulse-motor ignition control logicJournal of Guidance, Control, and Dynamics, 1987
- Maximum-information guidance for homing missilesJournal of Guidance, Control, and Dynamics, 1985
- Optimal controller for homing missileJournal of Guidance, Control, and Dynamics, 1985
- A new guidance law for homing missilesJournal of Guidance, Control, and Dynamics, 1985
- Status and concerns for bank-to-turn control of tactical missilesJournal of Guidance, Control, and Dynamics, 1985
- Target acceleration modeling for tactical missile guidanceJournal of Guidance, Control, and Dynamics, 1984
- Adaptive Kalman filter for tracking maneuvering targetsJournal of Guidance, Control, and Dynamics, 1983
- Comparison of Optimal Control and Differential Game Intercept Missile Guidance LawsJournal of Guidance and Control, 1981
- Guidance Laws for Short-Range Tactical MissilesJournal of Guidance and Control, 1981