東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

FindBook

Google Book

Amazon

博客來

Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations./
作者:	Benson, Conor J.
出版者:	Ann Arbor : ProQuest Dissertations & Theses, : 2021,
面頁冊數:	212 p.
附註:	Source: Dissertations Abstracts International, Volume: 83-03, Section: B.
Contained By:	Dissertations Abstracts International83-03B.
標題:	Aerospace engineering. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28647847
ISBN:	9798538153602

Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations.
Benson, Conor J.

Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations. - Ann Arbor : ProQuest Dissertations & Theses, 2021 - 212 p.

Source: Dissertations Abstracts International, Volume: 83-03, Section: B.

Thesis (Ph.D.)--University of Colorado at Boulder, 2021.

This item must not be sold to any third party vendors.

Reflection and thermal re-emission of solar radiation can influence the rotational dynamics of small bodies via the Yarkovsky-O'Keefe-Radzievskii-Paddack (YORP) effect. The YORP effect plays a primary role in the dynamical evolution of small asteroids. Modeling and observations indicate that many defunct high-altitude earth-orbiting satellites are also driven by the YORP effect. However, no comprehensive YORP studies for defunct satellites in general rotation have been conducted. Better understanding of defunct satellite spin state evolution would improve solar radiation pressure modeling for orbit prediction and facilitate active debris removal and satellite servicing which require accurate target attitude information. This work explores the long-term general (uniform and tumbling) rotational dynamics of defunct satellites subject to the YORP effect, internal energy dissipation, and gravity gradient torques through dynamical modeling and observation analysis. Focus is placed on the well-documented and dynamically interesting GOES 8-12 geosynchronous satellites. Full dynamics models are developed which illustrate rich, previously undocumented behavior including tumbling cycles, sun-tracking precession, tumbling period resonances, and asymptotically stable tumbling states/limit cycles. Using osculating rotational elements, the relevant perturbations are then analytically and numerically averaged over the satellite's general rotation, defined by Jacobi elliptic functions. These new tumbling-averaged models capture and explain the full dynamics behavior and reduce computation times by several orders of magnitude. The tumbling-averaged models facilitate broad exploration and classification of small body spin state evolution. Techniques for extracting spin state information from tumbling satellite light curve and Doppler radar observations are then developed. Analysis of GOES 8-12 observations from 2014 - 2020 reveals diverse, evolving spin states and clear consistencies with dynamical theory. The averaged models are then applied to box-wing satellites and meter-sized asteroids.

ISBN: 9798538153602Subjects--Topical Terms:

1002622
Aerospace engineering.
Subjects--Index Terms:

Attitude dynamics

Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations.
LDR:03321nmm a2200385 4500 001 2347643
005 20220823142320.5
008 241004s2021 ||||||||||||||||| ||eng d
020 $a 9798538153602
035 $a (MiAaPQ)AAI28647847
035 $a AAI28647847
040 $a MiAaPQ $c MiAaPQ
100 1 $a Benson, Conor J. $0 (orcid)0000-0003-3332-2164 $3 3686921
245 1 0 $a Solar Torque and Dissipation Dynamics for Tumbling Bodies: Theory and Observations.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2021
300 $a 212 p.
500 $a Source: Dissertations Abstracts International, Volume: 83-03, Section: B.
500 $a Advisor: Scheeres, Daniel.
502 $a Thesis (Ph.D.)--University of Colorado at Boulder, 2021.
506 $a This item must not be sold to any third party vendors.
520 $a Reflection and thermal re-emission of solar radiation can influence the rotational dynamics of small bodies via the Yarkovsky-O'Keefe-Radzievskii-Paddack (YORP) effect. The YORP effect plays a primary role in the dynamical evolution of small asteroids. Modeling and observations indicate that many defunct high-altitude earth-orbiting satellites are also driven by the YORP effect. However, no comprehensive YORP studies for defunct satellites in general rotation have been conducted. Better understanding of defunct satellite spin state evolution would improve solar radiation pressure modeling for orbit prediction and facilitate active debris removal and satellite servicing which require accurate target attitude information. This work explores the long-term general (uniform and tumbling) rotational dynamics of defunct satellites subject to the YORP effect, internal energy dissipation, and gravity gradient torques through dynamical modeling and observation analysis. Focus is placed on the well-documented and dynamically interesting GOES 8-12 geosynchronous satellites. Full dynamics models are developed which illustrate rich, previously undocumented behavior including tumbling cycles, sun-tracking precession, tumbling period resonances, and asymptotically stable tumbling states/limit cycles. Using osculating rotational elements, the relevant perturbations are then analytically and numerically averaged over the satellite's general rotation, defined by Jacobi elliptic functions. These new tumbling-averaged models capture and explain the full dynamics behavior and reduce computation times by several orders of magnitude. The tumbling-averaged models facilitate broad exploration and classification of small body spin state evolution. Techniques for extracting spin state information from tumbling satellite light curve and Doppler radar observations are then developed. Analysis of GOES 8-12 observations from 2014 - 2020 reveals diverse, evolving spin states and clear consistencies with dynamical theory. The averaged models are then applied to box-wing satellites and meter-sized asteroids.
590 $a School code: 0051.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Doppler radar. $3 1640878
650 4 $a Energy dissipation. $3 619627
650 4 $a Optical properties. $3 3560260
650 4 $a Light. $3 524021
650 4 $a Satellites. $3 924316
650 4 $a Equilibrium. $3 668417
650 4 $a Physics. $3 516296
650 4 $a Computational physics. $3 3343998
650 4 $a Mechanics. $3 525881
653 $a Attitude dynamics
653 $a Celestial mechanics
653 $a Doppler radar
653 $a Light curves
653 $a Space situational awareness
690 $a 0538
690 $a 0346
690 $a 0216
690 $a 0605
710 2 $a University of Colorado at Boulder. $b Aerospace Engineering. $3 1030473
773 0 $t Dissertations Abstracts International $g 83-03B.
790 $a 0051
791 $a Ph.D.
792 $a 2021
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=28647847