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Optimal symmetric flight studiesSeveral topics in optimal symmetric flight of airbreathing vehicles are examined. In one study, an approximation scheme designed for onboard real-time energy management of climb-dash is developed and calculations for a high-performance aircraft presented. In another, a vehicle model intermediate in complexity between energy and point-mass models is explored and some quirks in optimal flight characteristics peculiar to the model uncovered. In yet another study, energy-modelling procedures are re-examined with a view to stretching the range of validity of zeroth-order approximation by special choice of state variables. In a final study, time-fuel tradeoffs in cruise-dash are examined for the consequences of nonconvexities appearing in the classical steady cruise-dash model. Two appendices provide retrospective looks at two early publications on energy modelling and related optimal control theory.
Document ID
19850012866
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Weston, A. R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Menon, P. K. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Bilimoria, K. D.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Cliff, E. M.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Kelley, H. J.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-172508
NAS 1.26:172508
Report Number: NASA-CR-172508
Report Number: NAS 1.26:172508
Accession Number
85N21176
Funding Number(s)
PROJECT: RTOP 505-34-03
CONTRACT_GRANT: NAG1-203
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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