With recent advances in missile seekers and processors, and in the analysis of missile dynamics motions and the associated control subsystem designs, missile manoeuvre envelopes have significantly expanded. This symposium examined the stability and controllability of such missiles and provided a forum for discussing the different techniques currently involved in dealing with various aspects of this subject. The presentations ranged from prediction, simulation and test, through to a look at current development experience. The subject of the symposium was deliberately limited to tactical missiles, encompassing air-to-air, air-to-ground, and ground-to-air, but not ballistic missiles. Partial contents: Prediction of stability derivatives for missiles using the HISSS panel code; -- Missile DATACOM; -- Enhancements for design applications; Prediction of dynamic derivatives and of tactical missile dynamics; Vortex induced characteristics of missiles in unsteady maneuvers; Aeroelastic tailoring procedure for controlling fin hinge moments; Alternative polar homing strategies; How to control unstable missile airframes -- Methodology and Limitations; New test techniques to evaluate near field effects for supersonic store carriage and separation; Remote control missile model test; Wind tunnel tests -- The role of the model; Identification of stability and control parameters of a brilliant ammunition. NATO-furnished. (edc)


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