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This paper introduces a disturbance observer (DO) based reliable H∞ fuzzy attitude tracking control design for Mars entry vehicles with actuator failures.
This paper deals with the design of robust Fault Detection and Isolation (FDI) filters for atmospheric re-entry vehicles subjected to actuator faults.
A common PD-Mamdani fuzzy logic controller is designed for all the five re-entry flight regions characterized by different actuator configurations.
According to the most recent network time delay, the TDC selects just one entry of the control vector and applies it to the actuator through a zero order hold element.
The faulty door-lock actuator should be replaced.
Entry £5.
Free entry.
Entry fee?
Entry re.
A second large piece, an actuator for the right outboard elevon, was also found by searchers.
"Refused entry".
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