Algorithm for Optimal Flight Vehicle Design

Abstract

The book discusses algorithmic methods of planning of flight vehicles using electronic digital computers. One such method of optimal planning is developed and investigated, including a presentation of the variational problem (strict mathematical definition of the required conditions of optimization) considering analysis of the flight vehicle as a structure which receives various loads in flight, and as an object of control, plus an algorithm for its solution with a mathematical foundation for the algorithm itself. A multistage flight vehicle is used as an example to show the peculiarities of this algorithm when independent maneuver of the vehicle is possible after separation of initial stages or when the external and internal problems are analyzed together during interplanetary flights. In the algorithm, the criterion for improvement of the vehicle depends on the flight time, kinematic parameters of the vehicle at the end of the flight, its launch weight and the payload which it transports. Combining the theory of the variational problem and of the computer algorithm for its solution provides one with a logically complete algorithm for optimal planning of a vehicle.

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Document Details

Document Type
Technical Report
Publication Date
Jan 11, 1971
Accession Number
AD0720915

Entities

People

  • E. V. Tarasov

Organizations

  • Air Force Systems Command

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aerodynamic Heating
  • Algorithms
  • Artificial Intelligence
  • Ballistic Missiles
  • Boundary Layer
  • Combustion Chambers
  • Computational Science
  • Computer Programs
  • Computers
  • Control Systems
  • Convection
  • Differential Equations
  • Intermediate Range Ballistic Missiles
  • Theater Ballistic Missiles
  • Variational Equations

Fields of Study

  • Engineering

Readers

  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Space Exploration and Orbital Mechanics.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems