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.
(a) |
(b) |
(c) |
(d) |