Results 31 to 40 of about 7,088 (161)
ObjectiveThe causal factors underlying anomalies during carrier-based aircraft launch and recovery are often rare and unpredictable. To address the hallucination issues commonly encountered by large language models (LLMs) when generating these anomaly ...
Zhengqing HU +7 more
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Aircraft Spin Recovery Technique Based on Deep Reinforcement Learning [PDF]
This paper builds an aircraft simulation environment, and establishes a test model of an automated spin recovery algorithm based on proximal policy optimization (PPO) algorithm.
Tan Jianmei, Wang Junqiu
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An aircraft carrier's formidable combat capability relies on sorties, with efficient deck operations as the core to enhance sortie and recovery capabilities.
Wei Han +4 more
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Since child aircraft are significantly impacted by the wake interference from the mother aircraft during aerial refueling or the autonomous recovery of unmanned aerial vehicles(UAVs), a rapid prediction model for dual‑aircraft aerodynamic interference is
YUE Hao +4 more
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Thermodynamic analysis of a new electric environmental control system with energy recovery turbine
A new electric environmental control system for aircraft is investigated to promote the electrification of aircraft, focusing on energy recovery from the exhaust air.
Takahiro ADACHI +4 more
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Aircraft Route Recovery Based on An Improved GRASP Method
Aircrafts maintenance, temporary airport closures are common factors that disrupt normal flight schedule. The aircraft route recovery aims to recover original schedules by some strategies, including flights swaps, and cancellations, which is a NP-hard ...
Yang He, Jinfu Zhu, Qiang Gao, Bo Zhu
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It is known that the identification performance of a multi-aircraft formation (MAF) of narrowband radar mainly depends on the time on target (TOT).
Yuan Jiang +5 more
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Wind Tunnel Experiment and Numerical Simulation of Secondary Flow Systems on a Supersonic Wing
Aircraft secondary flow systems are small-flow circulation devices that are used for thermal and cold management, flow control, and energy generation on aircraft. The aerodynamic characteristics of main-flow-based inlets have been widely studied, but the
Sheng Zhang +6 more
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For the time being, a combat-capable trainer aircraft has already been used as a light attack aircraft. The quality of mission effectiveness evaluation depends on the degree of relevance of mathematical models used.
S. A. Popov, Y. A. Gondarenko
doaj
The highly dynamic nature, strong uncertainty, and coupled multiple safety constraints inherent in carrier aircraft recovery operations pose severe challenges for real-time decision-making.
Wei Han +6 more
doaj +1 more source

