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An Investigation Into Optimal Descent Trajectories for Multipurpose Long Range Space Vehicles Under Advanced Conditions.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	An Investigation Into Optimal Descent Trajectories for Multipurpose Long Range Space Vehicles Under Advanced Conditions./
作者:	Levis, John M.
面頁冊數:	1 online resource (127 pages)
附註:	Source: Masters Abstracts International, Volume: 85-01.
Contained By:	Masters Abstracts International85-01.
標題:	Aerospace engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9798379953850

An Investigation Into Optimal Descent Trajectories for Multipurpose Long Range Space Vehicles Under Advanced Conditions.
Levis, John M.

An Investigation Into Optimal Descent Trajectories for Multipurpose Long Range Space Vehicles Under Advanced Conditions. - 1 online resource (127 pages)

Source: Masters Abstracts International, Volume: 85-01.

Thesis (M.S.)--The University of Texas Rio Grande Valley, 2023.

Includes bibliographical references

In this work, we investigate the problem of fuel-optimal control of space vehicle descent trajectories. The main tool we use to establish optimality is Pontryagin's Maximum Principle. We present a variety of scenarios with increasing complexities, including drag, wind, and moving landing platforms in the context of differing atmospheric and gravitational conditions. Throughout the paper, we use a balance of analytical and numerical techniques. Finally, observations and conclusions drawn from the investigation form the basis for suggestions into additional areas of analysis.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798379953850Subjects--Topical Terms:

686400
Aerospace engineering.
Subjects--Index Terms:

Gravitational conditionsIndex Terms--Genre/Form:

554714
Electronic books.

An Investigation Into Optimal Descent Trajectories for Multipurpose Long Range Space Vehicles Under Advanced Conditions.
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504 $a Includes bibliographical references
520 $a In this work, we investigate the problem of fuel-optimal control of space vehicle descent trajectories. The main tool we use to establish optimality is Pontryagin's Maximum Principle. We present a variety of scenarios with increasing complexities, including drag, wind, and moving landing platforms in the context of differing atmospheric and gravitational conditions. Throughout the paper, we use a balance of analytical and numerical techniques. Finally, observations and conclusions drawn from the investigation form the basis for suggestions into additional areas of analysis.
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538 $a Mode of access: World Wide Web
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650 4 $a Applied mathematics. $3 1069907
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653 $a Space vehicles
653 $a Trajectories
653 $a Landing platforms
653 $a Complexities
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