國立虎尾科技大學 |

Rigid body dynamics for space applications

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Rigid body dynamics for space applications/ Vladimir S. Aslanov.
作者:	Aslanov, V. S.
出版者:	Oxford :Butterworth-Heinemann, : 2017.,
面頁冊數:	1 online resource (420 p.) :ill. :
標題:	Space sciences. -
電子資源:	https://www.sciencedirect.com/science/book/9780128110942
ISBN:	9780081018743 (electronic bk.)

Rigid body dynamics for space applications
Aslanov, V. S.

Rigid body dynamics for space applications[electronic resource] /Vladimir S. Aslanov. - Oxford :Butterworth-Heinemann,2017. - 1 online resource (420 p.) :ill.

Includes bibliographical references and index.

Mathematical Mechanical Preliminaries --Machine generated contents note:

ISBN: 9780081018743 (electronic bk.)

Nat. Bib. No.: GBB850478bnbSubjects--Topical Terms:

715034
Space sciences.
Index Terms--Genre/Form:

554714
Electronic books.

LC Class. No.: QA861 / .A75 2017

Dewey Class. No.: 629.47/1

Rigid body dynamics for space applications
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007 cr |n|||||||||
008 221013s2017 enka ob 001 0 eng d
015 $a GBB850478 $2 bnb
020 $a 9780081018743 (electronic bk.)
020 $a 0081018746 (electronic bk.)
020 $a 9780128110942
035 $a 020877708
040 $a Uk $b eng $c Uk
041 0 $a eng
050 4 $a QA861 $b .A75 2017
082 0 0 $a 629.47/1 $2 23
100 1 $a Aslanov, V. S. $q (Vladimir Stepanovich) $3 1028609
245 1 0 $a Rigid body dynamics for space applications $h [electronic resource] / $c Vladimir S. Aslanov.
260 $a Oxford : $b Butterworth-Heinemann, $c 2017.
300 $a 1 online resource (420 p.) : $b ill.
504 $a Includes bibliographical references and index.
505 0 0 $g Machine generated contents note: $g 1. $t Mathematical Mechanical Preliminaries -- $g 1.1. $t Mathematics -- $g 1.2. $t Rigid Body Kinematic -- $g 1.3. $t Rigid Body Dynamics -- $g 1.4. $t Chaotic Motion -- $t References -- $g 2. $t Reentry Attitude Dynamics -- $g 2.1. $t Introduction -- $g 2.2. $t Aerodynamics of Reentry Vehicles -- $g 2.3. $t The Equations of Motion -- $g 2.4. $t Analytical Solutions of the Undisturbed Equation for Sinusoidal Aerodynamic Moment -- $g 2.5. $t Analytical Solutions of the Undisturbed Equation for Biharmonical Aerodynamic Moment -- $g 2.6. $t Quasistatic Solutions for the Disturbed Equation of Motion -- $g 2.7. $t Adiabatic Invariants and the Approximate Solution for the Disturbed Motion -- $g 2.8. $t Bifurcation and Ways of Its Elimination at the Descent of Spacecraft in the Rarefied Atmosphere -- $g 2.9. $t Chaotic Attitude Motion of Reentry Vehicle With an Internal Moving Mass -- $g 2.10. $t Chaotic Behavior of Bodies in a Resistant Medium -- $g 2.11.
505 0 0 $t Chaotic Motion of a Reentry Capsule During Descent into the Atmosphere -- $t References -- $g 3. $t Dynamics and Control of Coaxial Satellite Gyrostats -- $g 3.1. $t Introduction -- $g 3.2. $t Attitude Motion Equations -- $g 3.3. $t Integrable Cases in the Dynamics of Coaxial Gyrostats -- $g 3.4. $t The Exact Analytical Solutions -- $g 3.5. $t Dynamics and Chaos Control of the Gyrostats -- $g 3.6. $t Dynamics and Control of Dual-Spin Gyrostat Spacecraft With Changing Structure -- $g 3.7. $t Adiabatic Invariants in the Dynamics of Axial Gyrostats -- $t References -- $g 4. $t Deployment, Dynamics, and Control of a Tether-Assisted Return Mission of a Reentry Capsule -- $g 4.1. $t Introduction -- $g 4.2. $t Mathematical Model of a Satellite With a Tethered Payload -- $g 4.3. $t Analytical Solution in the Case of a Slow Changing of the Parameters -- $g 4.4. $t Oscillations of the Satellite With a Vertical Elastic Tether -- $g 4.5. $t Oscillations in the Case of an Elliptic Orbit -- $g 4.6.
505 0 0 $t Swing Principle for Deployment of a Tether-Assisted Return Mission of a Reentry Capsule -- $g 4.7. $t Tether-Assisted Return Mission From an Elliptical Orbit Taking Into Account Atmospheric Stage of Reentry -- $t References -- $g 5. $t Removal of Large Space Debris by a Tether Tow -- $g 5.1. $t Introduction -- $g 5.2. $t Dynamics of Orbital Debris Connected to Spacecraft by a Tether in a Free Space -- $g 5.3. $t Dynamics of Large Orbital Debris Removal Using Tethered Space Tug in the Earth's Gravitational Field -- $g 5.4. $t Behavior of Tethered Debris With Flexible Appendages -- $g 5.5. $t Dynamics, Analytical Solutions and Choice of Parameters for Towed Space Debris With Flexible Appendages -- $g 5.6. $t The Motion of Tethered Tug-Debris System With Fuel Residuals -- $g 5.7. $t Dynamics of Towed Large Space Debris Taking Into Account Atmospheric Disturbance -- $g 5.8. $t Chaos Behavior of Space Debris During Tethered Tow -- $t References -- $g 6. $t Original Tasks of Space Mechanics -- $g 6.1.
505 0 0 $t Introduction -- $g 6.2. $t Gravitational Stabilization of the Satellite With a Moving Mass -- $g 6.3. $t The Dynamics of the Spacecraft of Variable Composition -- $g 6.4. $t Restoration of Attitude Motion of Satellite Using Small Numbers of Telemetry Measurements -- $t References.
650 0 $a Space sciences. $3 715034
650 0 $a Dynamics, Rigid. $3 528260
655 4 $a Electronic books. $2 local $3 554714
856 4 0 $u https://www.sciencedirect.com/science/book/9780128110942