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

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.

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Document Details

Document Type
Technical Report
Publication Date
Dec 27, 1995
Accession Number
ADA308105

Entities

People

  • Blaise Morton
  • Mike Elgersma

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Algorithms
  • Closed Loop Systems
  • Computational Science
  • Computations
  • Control Systems
  • Control Systems Engineering
  • Geometric Forms
  • Geometry
  • Guidance
  • Navigation
  • Open Loop Systems
  • Operating Systems
  • Proportional Navigation
  • Three Dimensional
  • Trajectories
  • Two Dimensional

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Missile Defense Systems.