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Special control mode in the problem of optimal turn of an arbitrary rigid body (spacecraft)
| Content Provider | Semantic Scholar |
|---|---|
| Author | Molodenkov, A. V. Sapunkov, Ya. G. |
| Copyright Year | 2012 |
| Abstract | The problem of optimal turn of spacecraft as a rigid body of arbitrary dynamic configuration under arbitrary boundary conditions with respect to angular position and angular velocity of spacecraft in the quaternion formulation is considered. The optimality criterion is a functional that combines time and the integral value of the control vector magnitude spent for the spacecraft turn. A special control mode of the spacecraft is studied. Examples of calculations are given. |
| Starting Page | 306 |
| Ending Page | 314 |
| Page Count | 9 |
| File Format | PDF HTM / HTML |
| DOI | 10.1134/S1064230712010121 |
| Volume Number | 51 |
| Alternate Webpage(s) | https://page-one.springer.com/pdf/preview/10.1134/S1064230712010121 |
| Alternate Webpage(s) | https://doi.org/10.1134/S1064230712010121 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |