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Near-optimal energy transitions for energy-state trajectories of hypersonic aircraftA problem of the instantaneous energy transition that occurs in energy-state approximation is considered. The transitions are modeled as a sequence of two load-factor bounded paths (either climb-dive or dive-climb). The boundary-layer equations associated with the energy-state dynamic model are analyzed to determine the precise location of the transition.
Document ID
19930029279
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ardema, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Bowles, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Terjesen, E. J. (NASA Ames Research Center Moffett Field, CA, United States)
Whittaker, T. (Sterling Software, Inc. Palo Alto, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 92-4300
Meeting Information
Meeting: AIAA, Guidance, Navigation and Control Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 10, 1992
End Date: August 12, 1992
Sponsors: AIAA
Accession Number
93A13276
Distribution Limits
Public
Copyright
Other

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