Research Article
Sliding Mode Control for Mass Moment Aerospace Vehicles Using Dynamic Inversion Approach
Table 1
Rule-table of FSMC.
| , | ā | , | ā | NB | NS | ZO | PS | PB |
| , | NB | PB | PB | PS | PS | ZO | NS | PB | PS | PS | ZO | ZO | ZO | PS | PS | ZO | ZO | NS | PS | PS | ZO | ZO | NS | NS | PB | ZO | ZO | NS | NS | NB |
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