| contributor author | D. E. Hill | |
| contributor author | J. R. Baumgarten | |
| date accessioned | 2017-05-08T23:37:53Z | |
| date available | 2017-05-08T23:37:53Z | |
| date copyright | December, 1992 | |
| date issued | 1992 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26187#728_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109931 | |
| description abstract | Spin-stabilized spacecraft with sloshing fluid stores are known to be a source of dynamic instability for certain spacecraft configurations. A time varying linear feedback control law was developed, using an equivalent spherical pendulum mechanical model of the fluid motion coupled to the main body dynamics, which stabilizes the highly nonlinear dynamic system within a large region of operation. The control law was also demonstrated to perform a pointing maneuver. A control design for a specific spacecraft is outlined and implemented by sensing only the main body angular rates and attitude. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Control of Spin-Stabilized Spacecraft With Sloshing Fluid Stores | |
| type | Journal Paper | |
| journal volume | 114 | |
| journal issue | 4 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.2897749 | |
| journal fristpage | 728 | |
| journal lastpage | 731 | |
| identifier eissn | 1528-9028 | |
| keywords | Particle spin | |
| keywords | Fluids | |
| keywords | Sloshing | |
| keywords | Space vehicles | |
| keywords | Motion | |
| keywords | Design | |
| keywords | Feedback | |
| keywords | Nonlinear dynamical systems | |
| keywords | Pendulums AND Dynamics (Mechanics) | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;1992:;volume( 114 ):;issue: 004 | |
| contenttype | Fulltext | |