Burn Phase Corrections of Maneuver Ballistic Missiles with Star Light

Abstract

In this paper, the maneuver ballistic missile parametric correction in the burning phase with star light is studied, when the maneuver ballistic missile is launched under the condition that the initial position is not exactly defined and the inertial navigation platform is not completely leveled and aligned.

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Document Details

Document Type
Technical Report
Publication Date
Dec 03, 1991
Accession Number
ADA254105

Entities

People

  • Gongxun Shen
  • Zhiming Zhou

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Ballistic Missiles
  • Celestial Navigation
  • Coordinate Systems
  • Equations
  • Euler Angles
  • Foreign Technology
  • Gravitational Fields
  • Grids
  • Guidance
  • Inertial Navigation
  • Latitude
  • Measurement
  • Navigation
  • Observation
  • Platforms
  • Stabilized Platforms
  • Standards

Fields of Study

  • Physics

Readers

  • Inertial Navigation Systems.
  • Optical Physics and Photonics.
  • Space Exploration and Orbital Mechanics.