Progress in Estimation and Control for Air-Launched Missiles. Part 1. A Real-Time3D Mini-Max Pursuit-Evader Algorithm, Part 2. Estimation

摘要

Part I of this report describes a real time three dimensional minimax pursuitevader algorithm. The fast algorithm is possible due to the assumption of constant speed, piecewise circular trajectories. Part II of this report includes several papers on the interaction of estimation and control for missile guidance.