International Journal of Aerospace Engineering / 2016 / Article / Fig 16

Research Article

Dynamics and Control of a Tethered Satellite System Based on the SDRE Method

Figure 16

Libration angles from the formulations based on point by applying the SDRE control with for (a) the first 10 orbits and (b) the first 0.1 orbits.
(a)
(b)

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