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Co-Self-Assembled Interface Engineering Assisted for Bend-Resistant and Efficient Flexible Perovskite Solar Cells. [PDF]
Wang C +16 more
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Review of Hydrogen Sensors in Aerobic and Anaerobic Environments Coupled with Artificial Intelligence Tools. [PDF]
Herbeck-Tazibt J +3 more
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Durable Superhydrophobic Composite Coating Based on Hydrangea-like SiO<sub>2</sub> Nanoparticles with Excellent Performance in Anticorrosion, Drag Reduction, and Antifouling. [PDF]
Xue Y +7 more
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Carrier-Based Aircraft Steam Catapult Control System
2018 37th Chinese Control Conference (CCC), 2018In order to make the carrier-based aircraft take off smoothly, a steam catapult controller is designed in this paper. The thermodynamic model of the capacity selector valve, the steam storage cylinder and the cylinder, and the motion model of the carrier-based aircraft are built. Then the steam catapult controller is designed.
Chengtao Cai +4 more
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Future Carrier-Based Tactical Aircraft Study
1996A-961330;NASA Technical Memorandum ...
Samuels, Jeffery J. +5 more
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The Longitudinal Control Strategy Design of Carrier-based Aircraft
2018 IEEE CSAA Guidance, Navigation and Control Conference (CGNCC), 2018In order to solve the problem of the coupling of attitude and trajectory in the longitudinal channel at the end of carrier landing, a decoupling control strategy is proposed in this paper which uses the elevator channel to control the attitude and the engine channel to control the trajectory.
Tao Chen, Chuntao Li, Donghong Zhao
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Research on Landing Environment System of Carrier-Based Aircraft
2019 Chinese Control And Decision Conference (CCDC), 2019To guarantee the safety of carrier-based aircraft, the landing environment system has been researched in this paper. After being familiar with deck landing geometry, we model the aircraft carrier motion, including deterministic model and random model. The transformation law of atmospheric disturbances has been analyzed.
Xiaodong Su +4 more
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Radar ranges for carrier-based AEW aircraft
Journal of Aircraft, 1981The intricate details of the initial flaw shape can be ignored in the first approximation, expecially since, upon incipient growth, the crack rapidly attains a stable configuration (normally semicircular, semielliptic, etc., depending on the stress distribution).
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