| contributor author | Jianjun Shi | |
| contributor author | Atul G. Kelkar | |
| date accessioned | 2017-05-09T00:23:09Z | |
| date available | 2017-05-09T00:23:09Z | |
| date copyright | July, 2007 | |
| date issued | 2007 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26397#559_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135451 | |
| description abstract | This technical brief presents a nonlinear dynamic model of Jupiter Icy Moons Orbiter (JIMO), a concept design of a spacecraft intended to orbit the three icy moons of Jupiter, namely, Europa, Ganymede, and Callisto. The work presented in this paper represents a part of a feasibility study conducted to assess control requirements of the JIMO mission. A nonlinear dynamic model of JIMO is derived that includes rigid body as well as flexible body dynamics. A nonlinear dissipative control law with guaranteed stability is used to perform a representative in-orbit maneuver. The results presented are part of an exhaustive study conducted to evaluate various controller designs. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Dissipative Control Design for Jupiter Icy Moons Orbiter | |
| type | Journal Paper | |
| journal volume | 129 | |
| journal issue | 4 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.2745888 | |
| journal fristpage | 559 | |
| journal lastpage | 565 | |
| identifier eissn | 1528-9028 | |
| keywords | Control equipment | |
| keywords | Design | |
| keywords | Space vehicles AND Dynamics (Mechanics) | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;2007:;volume( 129 ):;issue: 004 | |
| contenttype | Fulltext | |