Accession Number : ADA308105

Title :   Progress in Estimation and Control for Air-Launched Missiles. Part 1. A Real-Time 3D Mini-Max Pursuit-Evader Algorithm, Part 2. Estimation.

Descriptive Note : Final rept. 15 Aug 92-31 Oct 95,

Corporate Author : HONEYWELL TECHNOLOGY CENTER MINNEAPOLIS MN

Personal Author(s) : Elgersma, Mike ; Morton, Blaise

PDF Url : ADA308105

Report Date : 27 DEC 1995

Pagination or Media Count : 134

Abstract : Part I of this report describes a real time three dimensional minimax pursuit evader 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.

Descriptors :   *ALGORITHMS, *GUIDED MISSILE TRAJECTORIES, *PURSUIT COURSES, *AIR LAUNCHED, VELOCITY, GUIDED MISSILES, EQUATIONS OF MOTION, REAL TIME, ALGEBRA, ESTIMATES, THREE DIMENSIONAL, GUIDANCE, EVASION, FLOATING POINT OPERATION, CIRCULAR.

Subject Categories : Guided Missile Traj, Accuracy and Ballistics
      Air- and Space-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE