Preliminary Gemini B Guidance Equations for the MOL Mission.

Abstract

This report provides a description of the guidance equations that are planned for Module III of the Gemini B Computer Program. This module contains the ascent mode, including the Orbit Adjust capability and the Abort Retrotime Predict mode. The equations for the latter are not included in this report. The main logic flow of the equations presented, however, is compatible with, and provides entrance and exit to and from, the Abort Retrotime Predict mode. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0856690

Entities

People

  • A. A. Linquiti
  • W. L. Hayden

Organizations

  • The Aerospace Corporation

Tags

DTIC Thesaurus Topics

  • Computer Programs
  • Computers
  • Equations
  • Guidance

Readers

  • Aerospace Propulsion Engineering.
  • Computer Science.
  • Missile Defense Systems.

Technology Areas

  • Space