Realization of Target Satellite Interception with Velocity-Gain Guidance.

Abstract

This paper is about the study of realization of the target satellite interception method with velocity gain guidance. The characteristics are the following: based on the given conditions of the interceptor's initial motion parameters and the target's trajectory parameters, firstly the predictive point of impact intercepting the target under the influence of J2 item of the earth oblatness is determined, then the interceptor's velocity required during the collision time using Lambert method is decided, at last, the target interception with velocity gain guidance method is realized. A transform condition with higher precision to the terminal guidance by using this method is guaranteed.

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Document Details

Document Type
Technical Report
Publication Date
Mar 22, 1996
Accession Number
ADA306519

Entities

People

  • Jia Peiran
  • Tang Guojian

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Air Intelligence
  • Artificial Satellites
  • Chinese Language
  • Computations
  • Coordinate Systems
  • Equations
  • Errors
  • Guidance
  • Interception
  • Microfiche
  • Perturbation Theory
  • Relative Motion
  • Simulations
  • Standards
  • Terminal Guidance
  • Trajectories

Readers

  • Control Systems Engineering.
  • Missile Defense Systems.
  • Space Exploration and Orbital Mechanics.

Technology Areas

  • Space
  • Space - Orbital Debris
  • Space - Spacecraft Maneuvers