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Analytical solutions to a guidance problem

  • J. E. Cochran
  • , T. S. No
  • , D. G. Thaxton
  • Auburn University
  • Air Force Research Laboratory

Research output: Contribution to journalJournal articlepeer-review

Abstract

Analytical solutions to the nonlinear equations of relative motion of a constant-velocity target and an interceptor that uses a form of proportional navigation as a guidance law are obtained for navigation gains of 3 and 4. The solutions, in terms of elliptic functions and integrals, are new closed-form solutions to a much investigated guidance problem and, although relatively complicated, may be readily evaluated. An additional result is a condition for intercept that is based on the initial conditions. Numerical results for an exoatmospheric intercept example are included.

Original languageEnglish
Pages (from-to)117-122
Number of pages6
JournalJournal of Guidance, Control, and Dynamics
Volume14
Issue number1
DOIs
StatePublished - 1991.01

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