Method of Guiding an In-Flight Vehicle to a Designed Flight Path.

Abstract

This patent application relates generally to guidance techniques and more particularly to a method of guiding an in-flight vehicle from its initial flight path at target acquisition to a desired flight path prior to target interception. A method of using two diverts in combination to guide an in-flight vehicle from its initial flight path at target acquisition to a desired flight path prior to target interception is provided. The two diverts are of known and different magnitudes. The magnitude of an initial projected miss at a closest approach to the target is used to determine the order and timing of the two diverts. At the completion of the second divert, the vehicle is on the desired flight path which may be either a collision or offset course trajectory as required by the vehicle's terminal guidance law.

Document Details

Document Type
Technical Report
Publication Date
Feb 27, 1991
Accession Number
ADD015061

Entities

People

  • Roger L. Gray

Organizations

  • United States Department of the Navy

Tags

DTIC Thesaurus Topics

  • Acquisition
  • Collisions
  • Flight
  • Flight Paths
  • Guidance
  • Interception
  • Law
  • Patent Applications
  • Target Acquisition
  • Terminal Guidance
  • Trajectories

Fields of Study

  • Physics

Readers

  • Aviation Science / Aeronautics.
  • Radar Systems Engineering.
  • Regression Analysis.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers