Carrier-based aircraft landing energy storage
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6 FAQs about [Carrier-based aircraft landing energy storage]
What are the key technologies of carrier-based aircraft in the landing process?
Abstract: The key technologies of carrier-based aircraft in the landing process include deck motion prediction and compensation, radar noise suppression, disturbance suppression of aft flow and wave-off decision.
What are the main contributions of a carrier-based aircraft longitudinal automatic landing model?
The main contributions of the present paper are as follows: (1) A carrier-based aircraft longitudinal automatic landing mathematical model is designed that contains actuator faults and nonlinear terms; (2) An observer and fault-tolerant control algorithm are designed, which are realized in a collaborative approach. Fig. 1.
Can carrier-based aircraft be controlled in the landing process?
The study provides a theoretical reference for the control of carrier-based aircraft landing. Conferences > 2021 6th International Confer... The key technologies of carrier-based aircraft in the landing process include deck motion prediction and compensation, radar noise suppression, disturbance suppression of aft flow and wave-off decision.
What is the risk of landing a carrier based aircraft?
1. Introduction The landing of the carrier-based aircraft has a high-risk potential, as it is subject to disturbances from the deck movement and airwake turbulence, which may result in accidents with the limited landing area , , , .
Is automatic landing an inevitable trend in carrier-based aircraft landing?
On the contrary, there may be a serious collision risk with the stern of the carrier , , . Therefore, automatic landing is an inevitable trend in the development of carrier-based aircraft landing. The current automatic landing algorithms mainly focus on the landing state deviations.
Do carrier-based aircraft perform a landing task after executing a mission?
However, the carrier-based aircraft typically performs the landing task after executing a mission, which may cause significant changes in aircraft mass and potential fault associated with the mission. It is necessary to consider abnormal situations such as faults, state deviations, and nonlinearity of the equations of motion comprehensively.