LEADER 04434nam 22005413u 450 001 9911006598703321 005 20230802010940.0 010 $a0-486-14013-X 010 $a1-62198-601-2 035 $a(CKB)2550000001187448 035 $a(EBL)1901070 035 $a(MiAaPQ)EBC1901070 035 $a(Au-PeEL)EBL1901070 035 $a(CaONFJC)MIL566816 035 $a(OCoLC)868968056 035 $a(EXLCZ)992550000001187448 100 $a20141229d2012|||| u|| | 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSpacecraft Attitude Dynamics 205 $a1st ed. 210 $aNewburyport $cDover Publications$d2012 215 $a1 online resource (1137 p.) 225 1 $aDover Books on Aeronautical Engineering 300 $aDescription based upon print version of record. 311 08$a0-486-43925-9 311 08$a1-306-35565-6 327 $a3.7 Dynamics of a System of Rigid Bodies3.8 Problems; Chapter 4 Attitude Dynamics of a Rigid Body; 4.1 Basic Motion Equations; 4.2 Torque-Free Motion; R? Inertially Axisymmetrical; 4.3 Torque-Free Motion; R? Tri-inertial; 4.4 Stability of Motion for R?; 4.5 Motion of a Rigid Body Under Torque; 4.6 Problems; Chapter 5 Effect of Internal Energy Dissipation on the Directional Stability of Spinning Bodies; 5.1 Quasi-Rigid Body with an Energy Sink, R?; 5.2 Rigid Body with a Point Mass Damper, R? + R?; 5.3 Problems; Chapter 6 Directional Stability of Multispin Vehicles; 6.1 The R? + W? Gyrostat 327 $a6.2 Gyrostat with Nonspinning Carrier6.3 The Zero Momentum Gyrostat; 6.4 The General Case; 6.5 System of Coaxial Wheels; 6.6 Problems; Chapter 7 Effect of Internal Energy Dissipation on the Directional Stability of Gyrostats; 7.1 Energy Sink Analyses; 7.2 Gyrostats with Discrete Dampers; 7.3 Problems; Chapter 8 Spacecraft Torques; 8.1 Gravitational Torque; 8.2 Aerodynamic Torque; 8.3 Radiation Torques; 8.4 Other Environmental Torques; 8.5 Nonenvironmental Torques; 8.6 Closing Remarks; 8.7 Problems; Chapter 9 Gravitational Stabilization; 9.1 Context 327 $a9.2 Equilibria for a Rigid Body in a Circular Orbit9.3 Design of Gravitationally Stabilized Satellites; 9.4 Flight Experience; 9.5 Problems; Chapter 10 Spin Stabilization in Orbit; 10.1 Spinning Rigid Body in Orbit; 10.2 Design of Spin-Stabilized Satellites; 10.3 Long-Term Effects of Environmental Torques, and Flight Data; 10.4 Problems; Chapter 11 Dual-Stabilization in Orbit: Gyrostats and Bias Momentum Satellites; 11.1 The Gyrostat in Orbit; 11.2 Gyrostats with External Rotors; 11.3 Bias Momentum Satellites; 11.4 Problems; Appendix A Elements of Stability Theory; A.1 Stability Definitions 327 $aA.2 Stability of the OriginA.3 The Linear Approximation; A.4 Nonlinear Inferences from Infinitesimal Stability Properties; A.5 Liapunov's Method; A.6 Stability of Linear Stationary Mechanical Systems; A.7 Stability Ideas Specialized to Attitude Dynamics; Appendix B Vectrices; B.1 Remarks on Terminology; B.2 Vectrices; B.3 Several Reference Frames; B.4 Kinematics of Vectrices; B.5 Derivative with Respect to a Vector; Appendix C List of Symbols; C.1 Lowercase Symbols; C.2 Uppercase Symbols; C.3 Lowercase Greek Symbols; C.4 Uppercase Greek Symbols; C.5 Other Notational Conventions; References 327 $aErrata 330 $aPointing a satellite in the right direction requires an extremely complex system - one that describes the satellite's orientation and at the same time predicts and either uses or neutralizes external influences. From its roots in classical mechanics and reliance on stability theory to the evolution of practical stabilization ideas, Spacecraft Attitude Dynamics offers comprehensive coverage of environmental torques encountered in space; energy dissipation and its effects on the attitude stability of spinning bodies; motion equation for four archetypical systems derived and used repeatedly throu 410 0$aDover Books on Aeronautical Engineering 606 $aSpace vehicles - Attitude control systems 615 0$aSpace vehicles - Attitude control systems. 676 $a629.4742 700 $aHughes$b Peter C$01824859 801 0$bAU-PeEL 801 1$bAU-PeEL 801 2$bAU-PeEL 906 $aBOOK 912 $a9911006598703321 996 $aSpacecraft Attitude Dynamics$94392241 997 $aUNINA