DocumentCode :
487437
Title :
The Goddard Problem with Constrained Time-of-Flight
Author :
Tsiotras, Panagiotis ; Kelley, Henry J.
Author_Institution :
Graduate Student, Department of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
fYear :
1988
fDate :
15-17 June 1988
Firstpage :
1412
Lastpage :
1421
Abstract :
Presently studied is the problem of the vertical flight of a rocket in a resisting medium, with a constraint of isoperimetric type. Only the case of maximum range for given flight-time has been analyzed, but the methodology applies to other types of constraints as well, e.g., the minimum-time problem, due to Mayer reciprocity. Analysis shows that a one-parameter family of singular extremals is generated according to the value of time-of-flight. Three cases of switching structures have been found, varying with the specified duration of flight, with the most interesting case featuring appearance of a second full-thrust subarc at the departure from the singular subarc owing to a low value of the upper bound on the thrust.
Keywords :
Aerospace engineering; Calculus; Drag; Equations; Oceans; Optimal control; Propulsion; Rockets; Time factors; Upper bound;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1988
Conference_Location :
Atlanta, Ga, USA
Type :
conf
Filename :
4789942
Link To Document :
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