| 000 | 04561cam a2200577Ki 4500 | ||
|---|---|---|---|
| 001 | 9780429446580 | ||
| 003 | FlBoTFG | ||
| 005 | 20220509192954.0 | ||
| 006 | m o d | ||
| 007 | cr cnu---unuuu | ||
| 008 | 190207s2019 flu ob 001 0 eng d | ||
| 040 |
_aOCoLC-P _beng _erda _epn _cOCoLC-P |
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| 020 |
_a9780429446580 _q(electronic bk.) |
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| 020 |
_a0429446586 _q(electronic bk.) |
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| 020 |
_a9780429822131 _q(electronic bk. : EPUB) |
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| 020 |
_a0429822138 _q(electronic bk. : EPUB) |
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| 020 |
_a9780429822124 _q(electronic bk. : Mobipocket) |
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| 020 |
_a042982212X _q(electronic bk. : Mobipocket) |
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| 020 |
_a9780429822148 _q(electronic bk. : PDF) |
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| 020 |
_a0429822146 _q(electronic bk. : PDF) |
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| 020 | _z9781138331501 | ||
| 020 | _z1138331503 | ||
| 035 | _a(OCoLC)1084727049 | ||
| 035 | _a(OCoLC-P)1084727049 | ||
| 050 | 4 |
_aTL3260 _b.Y36 2019eb |
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| 072 | 7 |
_aTEC _x009000 _2bisacsh |
|
| 072 | 7 |
_aTEC _x009070 _2bisacsh |
|
| 072 | 7 |
_aTEC _x016000 _2bisacsh |
|
| 072 | 7 |
_aTQ _2bicssc |
|
| 082 | 0 | 4 |
_a629.47/42 _223 |
| 100 | 1 |
_aYang, Yaguang, _eauthor. |
|
| 245 | 1 | 0 |
_aSpacecraft modeling, attitude determination, and control : _bquaternion-based approach / _cYaguang Yang (US Nuclear Regulatory Commission, Office of Research, Rockville, Maryland, USA). |
| 264 | 1 |
_aBoca Raton, FL : _bCRC Press, _c2019. |
|
| 300 | _a1 online resource. | ||
| 336 |
_atext _btxt _2rdacontent |
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| 337 |
_acomputer _bc _2rdamedia |
||
| 338 |
_aonline resource _bcr _2rdacarrier |
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| 500 | _a"A science publishers book." | ||
| 505 | 0 | _aIntroduction -- Orbit dynamics and properties -- Rotational sequences and quaternion -- Spacecraft dynamics and modeling -- Space environment and disturbance torques -- Spacecraft attitude determination -- Astronomical vector measurements -- Spacecraft attitude estimation -- Spacecraft attitude control -- Spacecraft actuators -- Spacecraft control using magnetic torques -- Attitude maneuver and orbit-raising -- Attitude mpc control -- Spacecraft control using cmg -- Spacecraft rendezvous and docking. | |
| 520 | _aThis book discusses all spacecraft attitude control-related topics: spacecraft (including attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of its many merits. The book lays a brief, but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques, therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided. The book also includes attitude control in some special maneuvers, such as orbital-raising, docking and rendezvous, that are normally not discussed in similar books. Almost all design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics. | ||
| 588 | _aOCLC-licensed vendor bibliographic record. | ||
| 650 | 0 |
_aSpace vehicles _xAttitude control systems. |
|
| 650 | 0 | _aStability of space vehicles. | |
| 650 | 0 | _aRotational motion (Rigid dynamics) | |
| 650 | 0 | _aQuaternions. | |
| 650 | 0 | _aVector analysis. | |
| 650 | 7 |
_aTECHNOLOGY & ENGINEERING / Engineering (General) _2bisacsh |
|
| 650 | 7 |
_aTECHNOLOGY / Engineering / Mechanical _2bisacsh |
|
| 650 | 7 |
_aTECHNOLOGY / Industrial Design / General _2bisacsh |
|
| 856 | 4 | 0 |
_3Taylor & Francis _uhttps://www.taylorfrancis.com/books/9780429446580 |
| 856 | 4 | 2 |
_3OCLC metadata license agreement _uhttp://www.oclc.org/content/dam/oclc/forms/terms/vbrl-201703.pdf |
| 999 |
_c127511 _d127511 |
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