@article{09f7cad41ff74156a07c65814be5e8b1,
title = "Lifting-Wing Quadcopter Modeling and Unified Control",
keywords = "Control Allocation, Fixed Wing Aircraft, Flight Control, Flight Mechanics, Hybrid Unmanned Aerial Vehicle, Lifting Wing, Quadcopter, Tilt Rotor Wing, Unmanned Aerial Vehicle, Vertical Take off and Landing",
author = "Quan Quan and Shuai Wang and Wenhan Gao",
year = "2025",
month = mar,
doi = "10.2514/1.G008134",
language = "英语",
volume = "48",
pages = "689--699",
journal = "Journal of Guidance, Control, and Dynamics",
issn = "0731-5090",
publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",
number = "3",
}