Multipoint optimal control with applications to space flight

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Abstract/Contents

Abstract
Pontryagin's Maximum Principle is generalized to multipoint optimal control with a proof given that is based entirely on the original principle. Accommodations are made for interdependency of constraints and parametric representation of the dynamics and cost function. The approach naturally applies to impulsive as well as continuous control. Periodic optimal control is an important consequence. Cost sensitivity of the performance index is also proven and demonstrated to be useful in understanding and solving optimal control problems. Three applications from space flight are solved to demonstrate the theory: optimal attitude scheduling of an imaging satellite, optimization of impulsive orbital transfer, and finding periodic orbits near the Earth-Moon Lagrange points.

Description

Type of resource text
Form electronic resource; remote; computer; online resource
Extent 1 online resource.
Place California
Place [Stanford, California]
Publisher [Stanford University]
Copyright date 2019; ©2019
Publication date 2019; 2019
Issuance monographic
Language English

Creators/Contributors

Author Zorn, Alan H
Degree supervisor Lall, Sanjay
Degree supervisor West, Matt
Thesis advisor Lall, Sanjay
Thesis advisor West, Matt
Thesis advisor D'Amico, Simone
Degree committee member D'Amico, Simone
Associated with Stanford University, Department of Aeronautics and Astronautics.

Subjects

Genre Theses
Genre Text

Bibliographic information

Statement of responsibility Alan Hall Zorn.
Note Submitted to the Department of Aeronautics and Astronautics.
Thesis Thesis Ph.D. Stanford University 2019.
Location electronic resource

Access conditions

Copyright
© 2019 by Alan H Zorn
License
This work is licensed under a Creative Commons Attribution Non Commercial 3.0 Unported license (CC BY-NC).

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