OPTIMUM PROGRAMMING OF THE THRUST OF THE POWER UNIT WHEN THE FLIGHT TRAJECTORY IS GIVEN

Abstract

The problem is analyzed of determining the optimum programming of the power unit's thrust, which will guarantee reaching a certain integral characteristic of motion (for example, range of flight, initial weight, and time consumed in reaching goal of extremal value at a given trajectory. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 05, 1962
Accession Number
AD0271846

Entities

People

  • Ye. V. Tarasov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Computer Programming
  • Computing-Related Activities
  • Guarantees
  • Integrals
  • Trajectories

Readers

  • Mathematics or Statistics
  • Operations Research
  • Robotics and Automation.