Complexity / 2020 / Article / Fig 2

Research Article

Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array

Figure 2

Representations of the solar array’s mechanisms and torque models. (a) Spring-damper mechanism. (b) CCL mechanism. (c) Latch mechanism. (d) Torque model of the solar array.

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