NONLINEAR APPROACH TO THE DESIGN OF JET ENGINE CONTROL SYSTEMS

This work uses a multiple time scaling analysis of jet engine dynamics to derive a nonlinear minimum time control law. The ideas are based on concepts taken from singular perturbation theory. Further reductions in model order are permitted by this approach, which results in a feedback form for the control solution. Numerical results are given which compare the accuracy of the solution with open-loop solutions obtained using conjugate gradient and dynamic programming methods.

Media Info

  • Features: References;
  • Pagination: p. 1181

Subject/Index Terms

Filing Info

  • Accession Number: 00178474
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Report/Paper Numbers: 77CH1269-OCS Proceeding
  • Files: TRIS
  • Created Date: Aug 19 1978 12:00AM