Research Article
Adaptive Fuzzy Control for Attitude Stabilization of Spacecraft with Deployable Composite Laminated Solar Array
Table 3
Fuzzy rules of the fuzzy PD controller.
| Rule index | Rule statements |
| Rule 1 | If (E is N) and (EC is N), then (KP is P) and (KD is P) | Rule 2 | If (E is N) and (EC is Z), then (KP is P) and (KD is Z) | Rule 3 | If (E is N) and (EC is P), then (KP is N) and (KD is P) | Rule 4 | If (E is Z) and (EC is N), then (KP is Z) and (KD is P) | Rule 5 | If (E is Z) and (EC is Z), then (KP is Z) and (KD is Z) | Rule 6 | If (E is Z) and (EC is P), then (KP is Z) and (KD is P) | Rule 7 | If (E is P) and (EC is N), then (KP is N) and (KD is P) | Rule 8 | If (E is P) and (EC is Z), then (KP is P) and (KD is Z) | Rule 9 | If (E is P) and (EC is P), then (KP is P) and (KD is P) |
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