Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Rush Robinett"'
Publikováno v:
Proposed for presentation at the 20th Wind Integration Workshop held September 29-30, 2021 in Berlin, Germany.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e532b6928504f9769309ce3676ab98e3
https://doi.org/10.2172/1886759
https://doi.org/10.2172/1886759
Publikováno v:
Proposed for presentation at the 2oth wind integration workshop held September 29-30, 2021 in berlin, germany.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::67399e53846cf9306fddaf2295796f1f
https://doi.org/10.2172/1888131
https://doi.org/10.2172/1888131
Autor:
Rush Robinett, David Wilson
Publikováno v:
2006 IEEE International Conference on Control Applications.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b4381e6fd17aeece89694330072c9124
https://doi.org/10.1109/cca.2006.286216
https://doi.org/10.1109/cca.2006.286216
Publikováno v:
Guidance, Navigation, and Control Conference.
A novel method is presented to carry out near-minimum-time maneuvers of a spacecraft of unknown inertia. The formulation assumes the presence of three orthogonal reaction wheels located near the system mass center and oriented arbitrarily with respec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8b8108367c3c17effb0a133a4bb73153
https://doi.org/10.2514/6.1997-3480
https://doi.org/10.2514/6.1997-3480
Publikováno v:
35th Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6b7d1329f1a903022ea185dc7535dbf0
https://doi.org/10.2514/6.1997-784
https://doi.org/10.2514/6.1997-784
Publikováno v:
35th Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bafc9b399b0638c0421dc011b50b77c6
https://doi.org/10.2514/6.1997-788
https://doi.org/10.2514/6.1997-788
Publikováno v:
35th Aerospace Sciences Meeting and Exhibit.
A generalized feedback control law design methodology is presented that applies to systems under control saturation constraints. Lyapunov stability theory is used to develop stable saturated control laws that can be augmentedtoanyunsaturatedcontrolla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e62a73332440eb134275b5f2eae51881
https://doi.org/10.2514/6.1997-112
https://doi.org/10.2514/6.1997-112
Conference
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Conference
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