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Aircraft trajectory optimization using singular perturbation methodsSingular perturbation methods are used to derive nonlinear feedback control laws for aircraft minimum time long range interception under the assumption of complete time scale separation. The resulting algorithms are in feedback form and can be implemented on a microcomputer for on-line trajectory optimization.
Document ID
19800066895
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mehra, R. K. (Scientific Systems, Inc. Cambridge, MA, United States)
Washburn, R. B., Jr. (Scientific Systems, Inc. Cambridge, Mass., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Annual Allerton Conference on Communication, Control, and Computing
Location: Monticello, IL
Start Date: October 10, 1979
End Date: October 12, 1979
Accession Number
80A51065
Funding Number(s)
CONTRACT_GRANT: NAS1-15113
Distribution Limits
Public
Copyright
Other

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