A STUDY OF TIME-OPTIMAL INTERCEPT IN TWO DIMENSIONS (VOL 2)

Abstract

A planar time-optimal formulation is used to study the terminal phase of interception above the atmosphere in a uniform gravitational field. The dependence on initial conditions of the optimal steering angle is examined for initial relative velocities ranging from 5,000 ft/sec to 50,000 ft/sec and initial distances up to 500,000 ft. Results are presented in graphical form for two typical rockets showing: (1) the range dependence of terminal error sensitivities to errors in measurements of initial conditions taken along the initial rectilinear coasting path and (2) the variation in these terminal error coefficients along optimal interception paths. Some interceptions with proportional control systems were made and compared with the optimal paths.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1965
Accession Number
AD0624219

Entities

People

  • Bernard H. Paiewonsky
  • Peter J. Woodrow

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Attitude Control Systems
  • Closed Loop Systems
  • Coefficients
  • Computational Science
  • Computer Programs
  • Control Systems
  • Coordinate Systems
  • Differential Equations
  • Dynamics
  • Equations
  • Flight Control Systems
  • Gravitational Fields
  • Interception
  • Line Of Sight
  • Measurement
  • Miss Distance

Fields of Study

  • Physics

Readers

  • Geodesy
  • Radar Systems Engineering.
  • Robotics and Automation.