Linear Dynamic Modeling of Satellites with Flexible Appendages
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Bester Preis: Fr. 24.76 (€ 25.32)¹ (vom 26.10.2019)1
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Linear Dynamic Modeling of Satellites with Flexible Appendages (2015)
DE PB NW RP
ISBN: 9783659395666 bzw. 3659395668, in Deutsch, LAP Lambert Academic Publishing Mrz 2015, Taschenbuch, neu, Nachdruck.
Von Händler/Antiquariat, AHA-BUCH GmbH [51283250], Einbeck, Germany.
This item is printed on demand - Print on Demand Titel. Neuware - This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,.etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS). 104 pp. Englisch.
This item is printed on demand - Print on Demand Titel. Neuware - This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,.etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS). 104 pp. Englisch.
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Symbolbild
Linear Dynamic Modeling of Satellites with Flexible Appendages (Paperback) (2015)
DE PB NW RP
ISBN: 9783659395666 bzw. 3659395668, in Deutsch, Omniscriptum Gmbh Co. Kg, Taschenbuch, neu, Nachdruck.
Lieferung aus: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, The Book Depository EURO [60485773], Slough, United Kingdom.
Language: English Brand New Book ***** Print on Demand *****.This book presents a method and a toolbox of Matlab Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks, .etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard s research labs in Ecole Nationale Superieure de l Aeronautique et de l Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
Von Händler/Antiquariat, The Book Depository EURO [60485773], Slough, United Kingdom.
Language: English Brand New Book ***** Print on Demand *****.This book presents a method and a toolbox of Matlab Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks, .etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard s research labs in Ecole Nationale Superieure de l Aeronautique et de l Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
3
Linear Dynamic Modeling of Satellites with Flexible Appendages
DE NW
ISBN: 9783659395666 bzw. 3659395668, in Deutsch, neu.
Lieferung aus: Deutschland, zzgl. Versandkosten.
This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,..etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,..etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
4
Linear Dynamic Modeling of Satellites with Flexible Appendages
~EN NW AB
ISBN: 9783659395666 bzw. 3659395668, vermutlich in Englisch, neu, Hörbuch.
Lieferung aus: Deutschland, Lieferzeit: 5 Tage.
This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,..etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
This book presents a method and a toolbox of Matlab & Simulink programs that are used to generate the dynamic model of a multi-body system for space applications. Two comprehensive examples of multi-body spacecraft along with their Matlab files are presented in this book. The multi-body system that is treated by this method, is composed of a main body (hub) with rigid and flexible bodies attached to it, such as solar panels, antennas, propellant tanks,..etc. The appendages can be connected to the hub by cantilever or pivot joints. In addition to that, the appendages can have an infinite number of flexible sub-attachments to them in an open mechanical chain. In this method, the rigid six degrees of freedom (three translational and three rotational) can be treated altogether. Every added pivot joint adds a degree of freedom to the system. The Matlab toolbox presented here, was completed as a masters project in Dr. D. Alazard's research labs in École Nationale Supérieure de l'Aéronautique et de l'Espace-Toulouse, France, for the purpose of aiding in the design of spacecraft Attitude and Orbit Control Systems (AOCS).
5
Linear Dynamic Modeling of Satellites with Flexible Appendages
~EN PB NW
ISBN: 3659395668 bzw. 9783659395666, vermutlich in Englisch, LAP Lambert Academic Publishing, Taschenbuch, neu.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
7
Linear Dynamic Modeling of Satellites with Flexible Appendages
EN NW
ISBN: 9783659395666 bzw. 3659395668, in Englisch, OmniScriptum GmbH & Co. KG, OmniScriptum GmbH & Co. KG, OmniScriptum GmbH & Co. KG, neu.
Lieferung aus: Vereinigte Staaten von Amerika, zzgl. Versandkosten, Free Shipping on eligible orders over $25.
Tantawi Khalid, Paperback, English-language edition, Pub by OmniScriptum GmbH & Co. KG.
Tantawi Khalid, Paperback, English-language edition, Pub by OmniScriptum GmbH & Co. KG.
8
Linear Dynamic Modeling of Satellites with Flexible Appendages (2015)
~EN PB NW
ISBN: 9783659395666 bzw. 3659395668, vermutlich in Englisch, Taschenbuch, neu.
Lieferung aus: Deutschland, Next Day, Versandkostenfrei.
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
Die Beschreibung dieses Angebotes ist von geringer Qualität oder in einer Fremdsprache. Trotzdem anzeigen
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