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A new formulation for the epsilon method applied to the minimum-time-to-climb problemBalakrishnan's epsilon technique is used to compute minimum-time profiles for the F-104 airplane. This technique differs from the classical gradient method in that a quadratic penalty on the error in satisfying the equation of motion is included in the cost function to be minimized as a means of eliminating the requirement of satisfying the equations of motion. Although the number of unknown independent functions is increased to include the state variables, the evaluation of the gradient of the cost function is simplified, resulting in considerable computational savings, thereby making it appear feasible to use the epsilon method for real-time application.
Document ID
19780015085
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Taylor, L. W., Jr.
(NASA Flight Research Center Edwards, CA, United States)
Smith, H. J.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA, Washington Fourth Inter-Center Control Systems Conf.
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78N23028
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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