مرور Volume 29, Issue 9 بر اساس موضوع "active landing gear"
در حال نمایش موارد 1 - 1 از 1
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Optimized Fuzzy Logic for Nonlinear Vibration Control of Aircraft Semi-active Shock Absorber with Input Constraint (TECHNICAL NOTE)
(Materials and Energy Research Center, 2016-09-01)Landing impact and runway unevenness have proximate consequence on performance of landing gear system and conduce to discomfort of passengers and reduction of the pilot’s capability to control aircraft. Finally, vibrations ...



