Research On Dynamic Model of Space Interceptor In End-Guidance Phase,

Abstract

This paper is intended to explain the realization of direct collision kill mode by space interceptor against a target. In accordance with the requirements of the interceptor guidance and control system program, an orbital control engine is proposed to make a modulation over interceptor centroid movement in the end guidance phase. Also, an attitude control engine is used to make an attitude adjustment. Furthermore, a six degree of freedom interceptor trajectory simulation model is constructed. The computational results of the model indicate that it is necessary and possible to achieve control over the interceptor by using attitude control and orbital control engines in the end guidance phase.

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Document Details

Document Type
Technical Report
Publication Date
Mar 08, 1996
Accession Number
ADA306494

Entities

People

  • Zheng Huimin

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Intelligence
  • Angular Momentum
  • Artificial Satellites
  • Attitude Control Systems
  • Collisions
  • Computations
  • Computers
  • Control Systems
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Guidance
  • Launch Vehicles
  • Orbits
  • Relative Motion
  • Simulations
  • Trajectories

Readers

  • Computational Modeling and Simulation
  • Marksmanship and Weaponry.
  • Robotics and Automation.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers