Funder
Nanjing University of Aeronautics and Astronautics State Key Laboratory of Mechanics and Control for Aerospace Structures
National Major Science and Technology Projects of China
National Natural Science Foundation of China
China Postdoctoral Science Foundation
Reference35 articles.
1. An optimization for alleviating pilot workload during tilt rotor aircraft conversion and reconversion maneuver;Yu;Aerosp. Sci. Technol.,2022
2. Research on integrated control of turboshaft engine based on required power prediction [Dissertation];Du,2023
3. Robust control for an unmanned helicopter with constrained flapping dynamics;Li;Chinese J. Aeronaut,2018
4. Flight simulation model application for AH-64A apache engine integration;Shanthakumaran,1993
5. Next generation control system for helicopter engines;Smith,2001
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