Optimal Trajectory Synthesis and Tracking Control for Spacecraft Large Attitude Manoeuvers
The classical approach to the problem of synthesizing an optimal attitude manoeuver trajectory, involves the use of the calculus of variations and the use Lagrange multipliers or co-states. The nonlinear large attitude manoeuver trajectory is controlled by a set of nonlinear evolving co-states. In t...
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| Formato: | Capítulo de libro |
| Lenguaje: | inglés |
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IntechOpen
2020
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| Materias: | |
| Acceso en línea: | https://www.intechopen.com/chapters/67273 |
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