OPTIMAL PROGRAM OF CORRECTION IN THE PROBLEM OF MOTION IN A GRAVITATIONAL FIELD WITH LIMITED POWER,

Abstract

The problem of optimal correction is formulated so that still before realization of the trajectory there are selected optimum, in the mean, weight relationships and optimum programs of rocket acceleration which will ensure maximum of payload on whose delivery it is possible to count on.

Document Details

Document Type
Technical Report
Publication Date
May 20, 1965
Accession Number
AD0615862

Entities

People

  • V. V. Tokarev

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Gravitational Fields
  • Gravity
  • Trajectories

Fields of Study

  • Physics

Readers

  • Control Systems Engineering.
  • Systems Analysis and Design