Design of Near-Optimal Guidance Law For Space Interception,

Abstract

The article applies an augmented linearization method for nonlinear systems to propose a near optimal control resolution method of secondary type index problems for nonlinear systems. This method is applied to design a near optimal terminal guidance law for space interception. As indicated in the simulation results, the near optimal guidance has good performance.

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Document Details

Document Type
Technical Report
Publication Date
Mar 21, 1996
Accession Number
ADA306504

Entities

People

  • Shi Xiaoping

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Intelligence
  • Control Systems
  • Equations
  • Error Analysis
  • Guidance
  • Interception
  • Line Of Sight
  • Linear Systems
  • Microfiche
  • Nonlinear Systems
  • Riccati Equation
  • Simulations
  • System Of Systems
  • Targets
  • Terminal Guidance
  • Terminals

Readers

  • Missile Defense Systems.
  • Operations Research

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers