Spin-Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels
A feedback control law that globally and asymptotically stabilizes a spacecraft about a revolute motion along a specified inertial axis is presented. After the spacecraft is stabilized, the command inputs of the feedback control law oscillate periodically to conserve the system angular momentum. In...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2001-09, Vol.24 (5), p.1046-1049 |
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| container_end_page | 1049 |
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| container_issue | 5 |
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| container_title | Journal of guidance, control, and dynamics |
| container_volume | 24 |
| creator | Kim, Sungpil Kim, Youdan |
| description | A feedback control law that globally and asymptotically stabilizes a spacecraft about a revolute motion along a specified inertial axis is presented. After the spacecraft is stabilized, the command inputs of the feedback control law oscillate periodically to conserve the system angular momentum. In general, there is no feedback control law that can be detunable and reorient the spacecraft simultaneously. |
| doi_str_mv | 10.2514/2.4818 |
| format | Article |
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Systems</subject><subject>Differential equations</subject><subject>Exact sciences and technology</subject><subject>Feedback control</subject><subject>Flight dynamics</subject><subject>Numerical methods</subject><subject>Reaction wheels</subject><subject>Rotation</subject><subject>Vectors</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2001</creationdate><recordtype>article</recordtype><recordid>eNqN0ctKw0AUBuBBFKxVnyGgqJvo3DOzlOINBMFWXA6nk5k6JU1iJsXq05uqWO1CXJ3Nx39uCO0TfEoF4Wf0lCuiNlCPCMZSphTfRD2cMZIKrPE22olxijFhkmQ9dDWsQ5meL0JMhi2MQxHeoA1VmVQ-geQ-TEKeDGuwzjbg2-QhhnKSjF6q5N6B_YCPT84VcRdteSii2_uqfTS6vBgNrtPbu6ubwfltClzrNhWgxyKHLBNeYNDUO8gZphnmjHrgICXOhZJ6zLlV3sJYg9I8V5Tk0BXWR8efsXVTPc9dbM0sROuKAkpXzaPJOM8IVkR28uhPSaWWQij8Hyg06-7XRwdrcFrNm7Lb1lBGmMKKSraKs00VY-O8qZswg-bVEGyW_zHULP_TwcOvOIgWCt9AaUP81kIqRSnt2MkngwDwo-NHiKlzb_y8KFq3aFcD_qZrfd8B8L2lig</recordid><startdate>20010901</startdate><enddate>20010901</enddate><creator>Kim, Sungpil</creator><creator>Kim, Youdan</creator><general>American Institute of Aeronautics and Astronautics</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>7TC</scope></search><sort><creationdate>20010901</creationdate><title>Spin-Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels</title><author>Kim, Sungpil ; Kim, Youdan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a499t-5a9b5da775f50a92fead30270432fa4a660d5869b44c8fcab9a894d821da4d83</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2001</creationdate><topic>Aerospace engineering</topic><topic>Applied sciences</topic><topic>Asymptotic stability</topic><topic>Computer science; control theory; systems</topic><topic>Control system synthesis</topic><topic>Control theory</topic><topic>Control theory. 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| fulltext | fulltext |
| identifier | ISSN: 0731-5090 |
| ispartof | Journal of guidance, control, and dynamics, 2001-09, Vol.24 (5), p.1046-1049 |
| issn | 0731-5090 1533-3884 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_26965580 |
| source | Alma/SFX Local Collection |
| subjects | Aerospace engineering Applied sciences Asymptotic stability Computer science control theory systems Control system synthesis Control theory Control theory. Systems Differential equations Exact sciences and technology Feedback control Flight dynamics Numerical methods Reaction wheels Rotation Vectors |
| title | Spin-Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels |
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