Spacecraft dynamics and control: the embedded model control approach
Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book...
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| Hauptverfasser: | , , , , |
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| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Cambridge, MA
Butterworth-Heinemann
[2018]
|
| Schlagworte: | |
| Online-Zugang: | FAW01 FLA01 Volltext Volltext Volltext |
| Zusammenfassung: | Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems |
| Beschreibung: | Includes bibliographical references and index |
| Beschreibung: | 1 online resource |
| ISBN: | 9780081017951 0081017952 |
Internformat
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| 245 | 1 | 0 | |a Spacecraft dynamics and control |b the embedded model control approach |c Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro |
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| 500 | |a Includes bibliographical references and index | ||
| 520 | |a Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems | ||
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| 700 | 1 | |a Massotti, Luca |4 aut | |
| 700 | 1 | |a Carlucci, Donato |4 aut | |
| 700 | 1 | |a Montenegro, Carlos Perez |4 aut | |
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Datensatz im Suchindex
| _version_ | 1804179235609247744 |
|---|---|
| any_adam_object | |
| author | Canuto, Enrico Novara, Carlo Massotti, Luca Carlucci, Donato Montenegro, Carlos Perez |
| author_facet | Canuto, Enrico Novara, Carlo Massotti, Luca Carlucci, Donato Montenegro, Carlos Perez |
| author_role | aut aut aut aut aut |
| author_sort | Canuto, Enrico |
| author_variant | e c ec c n cn l m lm d c dc c p m cp cpm |
| building | Verbundindex |
| bvnumber | BV045382986 |
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| dewey-full | 629.411 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.411 |
| dewey-search | 629.411 |
| dewey-sort | 3629.411 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| format | Electronic eBook |
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| id | DE-604.BV045382986 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T08:16:39Z |
| institution | BVB |
| isbn | 9780081017951 0081017952 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030769319 |
| oclc_num | 1028553070 |
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| physical | 1 online resource |
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| publishDate | 2018 |
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| publisher | Butterworth-Heinemann |
| record_format | marc |
| spelling | Canuto, Enrico Verfasser aut Spacecraft dynamics and control the embedded model control approach Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro Cambridge, MA Butterworth-Heinemann [2018] 1 online resource txt rdacontent c rdamedia cr rdacarrier Includes bibliographical references and index Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Space vehicles / Control systems fast Space vehicles / Dynamics fast Space vehicles Dynamics Space vehicles Control systems Dynamisches Verhalten (DE-588)4140475-0 gnd rswk-swf Lenkverhalten (DE-588)4167367-0 gnd rswk-swf Raumflugkörper (DE-588)4177066-3 gnd rswk-swf Lageregelung (DE-588)4034076-4 gnd rswk-swf Raumflugkörper (DE-588)4177066-3 s Dynamisches Verhalten (DE-588)4140475-0 s Lageregelung (DE-588)4034076-4 s Lenkverhalten (DE-588)4167367-0 s 1\p DE-604 Novara, Carlo aut Massotti, Luca aut Carlucci, Donato aut Montenegro, Carlos Perez aut Erscheint auch als Druck-Ausgabe 9780081007006 Erscheint auch als Druck-Ausgabe 0081007000 https://www.sciencedirect.com/science/book/9780081007006 Verlag URL des Erstveröffentlichers Volltext http://www.sciencedirect.com/science/book/9780081007006 Verlag URL des Erstveröffentlichers Volltext http://ezaccess.libraries.psu.edu/login?url=https://www.sciencedirect.com/science/book/9780081007006 Verlag URL des Erstveröffentlichers Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Canuto, Enrico Novara, Carlo Massotti, Luca Carlucci, Donato Montenegro, Carlos Perez Spacecraft dynamics and control the embedded model control approach TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Space vehicles / Control systems fast Space vehicles / Dynamics fast Space vehicles Dynamics Space vehicles Control systems Dynamisches Verhalten (DE-588)4140475-0 gnd Lenkverhalten (DE-588)4167367-0 gnd Raumflugkörper (DE-588)4177066-3 gnd Lageregelung (DE-588)4034076-4 gnd |
| subject_GND | (DE-588)4140475-0 (DE-588)4167367-0 (DE-588)4177066-3 (DE-588)4034076-4 |
| title | Spacecraft dynamics and control the embedded model control approach |
| title_auth | Spacecraft dynamics and control the embedded model control approach |
| title_exact_search | Spacecraft dynamics and control the embedded model control approach |
| title_full | Spacecraft dynamics and control the embedded model control approach Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro |
| title_fullStr | Spacecraft dynamics and control the embedded model control approach Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro |
| title_full_unstemmed | Spacecraft dynamics and control the embedded model control approach Enrico Canuto, Carlo Novara, Luca Massotti, Donato Carlucci, Carlos Perez Montenegro |
| title_short | Spacecraft dynamics and control |
| title_sort | spacecraft dynamics and control the embedded model control approach |
| title_sub | the embedded model control approach |
| topic | TECHNOLOGY & ENGINEERING / Engineering (General) bisacsh Space vehicles / Control systems fast Space vehicles / Dynamics fast Space vehicles Dynamics Space vehicles Control systems Dynamisches Verhalten (DE-588)4140475-0 gnd Lenkverhalten (DE-588)4167367-0 gnd Raumflugkörper (DE-588)4177066-3 gnd Lageregelung (DE-588)4034076-4 gnd |
| topic_facet | TECHNOLOGY & ENGINEERING / Engineering (General) Space vehicles / Control systems Space vehicles / Dynamics Space vehicles Dynamics Space vehicles Control systems Dynamisches Verhalten Lenkverhalten Raumflugkörper Lageregelung |
| url | https://www.sciencedirect.com/science/book/9780081007006 http://www.sciencedirect.com/science/book/9780081007006 http://ezaccess.libraries.psu.edu/login?url=https://www.sciencedirect.com/science/book/9780081007006 |
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