Designing of a Nonlinear Optimal Terminal Guidance Law for Space Interception,

Abstract

This article concerns a nonlinear kinematics model of space interception. Nonlinear optimal control is sought through use of inverse systematic methods. A theoretical nonlinear terminal guidance law of global state feedback is advanced. In addition, a simulation test is carried out and a comparison is made with proportional guidance. Results show that this guidance law performs satisfactorily.

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Document Details

Document Type
Technical Report
Publication Date
Oct 13, 1995
Accession Number
ADA300855

Entities

People

  • Shi Xiaoping
  • Wang Zicai

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Intelligence
  • Attitude Control Systems
  • Control Systems
  • Coordinate Systems
  • Equations
  • Equations Of Motion
  • Equations Of State
  • Guidance
  • Integral Equations
  • Interception
  • Line Of Sight
  • Linear Systems
  • Nonlinear Systems
  • Relative Motion
  • Simulations
  • Targets
  • Terminal Guidance

Readers

  • Adaptive Control and Estimation with Uncertainty in Dynamic Systems.
  • Sensor Fusion and Tracking Systems.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers