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 indexRule statements

Rule 1If (E is N) and (EC is N), then (KP is P) and (KD is P)
Rule 2If (E is N) and (EC is Z), then (KP is P) and (KD is Z)
Rule 3If (E is N) and (EC is P), then (KP is N) and (KD is P)
Rule 4If (E is Z) and (EC is N), then (KP is Z) and (KD is P)
Rule 5If (E is Z) and (EC is Z), then (KP is Z) and (KD is Z)
Rule 6If (E is Z) and (EC is P), then (KP is Z) and (KD is P)
Rule 7If (E is P) and (EC is N), then (KP is N) and (KD is P)
Rule 8If (E is P) and (EC is Z), then (KP is P) and (KD is Z)
Rule 9If (E is P) and (EC is P), then (KP is P) and (KD is P)