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pro vyhledávání: '"Lkay Yavrucuk"'
Publikováno v:
ACC
This paper presents a control algorithm for the autonomous landing of a fixed-wing aircraft. In the proposed approach, the classical PID control technique is augmented with a state-dependent coefficient (SDC) nonlinear model inversion. The SDC-based
Publikováno v:
Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power.
Hot-Gas Ingestion (HGI) to the engines can potentially occur when a rotorcraft or a VTOL/STOVL fixed-wing aircraft is operating in close proximity to the ground. Especially for helicopters, due to the rotor downwash hot exhaust gases get recirculated