Reentry Guidance System Studies.

Abstract

The report discusses the constraints imposed by 'dormancy' or rapid readiness upon reentry guidance systems and addresses: (1) Inflight alignment of the reentry inertial measurement unit with the booster inertial measurement unit; (2) progress in the derivation of instrument performance models; and (3) the development of a technique for obtaining single-level torquing by increasing instrument quantization with an 'interpolator'.

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1974
Accession Number
ADA006808

Entities

People

  • R. Carson
  • R. Setterlund
  • W. Mcfarland

Tags

DTIC Thesaurus Topics

  • Guidance
  • Inertial Measurement Units
  • Inertial Navigation
  • Inflight
  • Measurement
  • Navigation

Readers

  • Inertial Navigation Systems.
  • Missile Defense Systems.
  • Systems Analysis and Design