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Entry Guidance With Final State Targ...

Lee, Youngro,

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Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance // Youngro Lee.
Author:	Lee, Youngro,
Description:	1 electronic resource (147 pages)
Notes:	Source: Dissertations Abstracts International, Volume: 86-04, Section: B.
Contained By:	Dissertations Abstracts International86-04B.
Subject:	Aerospace engineering. -
Online resource:	https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31334896
ISBN:	9798384491606

Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance /
Lee, Youngro,

Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance /Youngro Lee. - 1 electronic resource (147 pages)

Source: Dissertations Abstracts International, Volume: 86-04, Section: B.

Propelled by humanity's ongoing space exploration, this dissertation studies atmospheric entry guidance, a critical technology for precise and safe planetary landings. A series of interconnected studies that explore the challenges and potential solutions in entry guidance is presented. Firstly, a comparative analysis of existing guidance laws and an extensive literature review facilitate two branches of entry guidance research. Secondly, a novel entry guidance law that can efficiently identify optimal entry trajectories for two types of entry missions is proposed based on optimal control theory. Thirdly, a thorough analysis of numerical predictor-corrector guidance (NPCG) reveals its limitations on energy management and provides a solution to address them. Fourthly, the NPCG technique is further improved to ensure it can generate entry trajectories precisely satisfying mission requirements. Examination and advancement of entry guidance capabilities presented in this study are expected to contribute to future planetary exploration efforts.

English

ISBN: 9798384491606Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Atmospheric entry guidance

Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance /
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245 1 0 $a Entry Guidance With Final State Targeting Capability Using Numerical Predictor-Corrector Guidance / $c Youngro Lee.
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300 $a 1 electronic resource (147 pages)
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500 $a Source: Dissertations Abstracts International, Volume: 86-04, Section: B.
500 $a Advisors: Lee, Dae-Young; Wie, Bong Committee members: Abdelkhalik, Ossama; Kumar, Ratnesh; Rossmanith, James.
502 $b Ph.D. $c Iowa State University $d 2024.
520 $a Propelled by humanity's ongoing space exploration, this dissertation studies atmospheric entry guidance, a critical technology for precise and safe planetary landings. A series of interconnected studies that explore the challenges and potential solutions in entry guidance is presented. Firstly, a comparative analysis of existing guidance laws and an extensive literature review facilitate two branches of entry guidance research. Secondly, a novel entry guidance law that can efficiently identify optimal entry trajectories for two types of entry missions is proposed based on optimal control theory. Thirdly, a thorough analysis of numerical predictor-corrector guidance (NPCG) reveals its limitations on energy management and provides a solution to address them. Fourthly, the NPCG technique is further improved to ensure it can generate entry trajectories precisely satisfying mission requirements. Examination and advancement of entry guidance capabilities presented in this study are expected to contribute to future planetary exploration efforts.
546 $a English
590 $a School code: 0097
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Astronomy. $3 517668
650 4 $a Atmospheric sciences. $3 3168354
653 $a Atmospheric entry guidance
653 $a Guidance and control
653 $a Mars entry descent and landing
653 $a Numerical predictor
653 $a Trajectory optimization
690 $a 0538
690 $a 0606
690 $a 0725
710 2 $a Iowa State University. $b Aerospace Engineering. $e degree granting institution. $3 3814666
720 1 $a Lee, Dae-Young $e degree supervisor.
720 1 $a Wie, Bong $e degree supervisor.
773 0 $t Dissertations Abstracts International $g 86-04B.
790 $a 0097
791 $a Ph.D.
792 $a 2024
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=31334896