Control Law of Terminal-Guidance Segment of Space Interceptors,

Abstract

The article discusses the control law of space single axis spin stabilized interceptors, relying on multiple solid fuel thruster engines for orbital control. By analyzing the motion law of the terminal guidance segment with mathematical simulation, an effective divergence control method with proportional guidance is derived. Moreover, the authors go on to discuss the principle of selecting various control parameters, and measures for reducing the off target amount, which have reference value in studying and developing similar types of space interceptors in China.

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Document Details

Document Type
Technical Report
Publication Date
Mar 27, 1996
Accession Number
ADA309746

Entities

People

  • Yang Yingbo
  • Zhou Huizhong

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Accuracy
  • Air Intelligence
  • Astronautics
  • Control Systems
  • Engines
  • Equations
  • Errors
  • Fuels
  • Guidance
  • Homing
  • Line Of Sight
  • Microfiche
  • Simulations
  • Solid Fuels
  • Target Seekers
  • Terminal Guidance

Readers

  • Missile Defense Systems.
  • Robotics and Automation.
  • Statistical inference.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers