Draft:Lifting-wing multicopter

• Comment: DO not resubmit without improvement. '''[[User:CanonNi]]''' (talk • contribs) 01:54, 17 May 2024 (UTC)

• Comment: Without more inline citations on factual statements to previous coverage using secondary and reliable sources, it is not possible to verify that this article is not WP:ORIGINAL RESEARCH. microbiologyMarcus ^{(petri dish·growths)} 16:02, 12 December 2023 (UTC)

---

The lifting-wing multicopter designed by the reliable flight control group of Beihang University

A lifting-wing multirotor is a combination of a lifting-wing and a multicopter. The plane of the rotor disc and lifting wing are installed at a fixed angle (for example, about 30-45 degrees), which greatly improves the forward flight efficiency while retaining the simple and reliable structure of multicopter and wind resistance. The unique layout significantly differs from conventional vertical takeoff and landing aircraft, such as tail-sitter and convertiplane. At present, almost all aircraft are in multicopter mode or fixed-wing mode most of the time, while the lifting-wing multicopter is always in the mixed phase of multicopter mode and fixed-wing mode. Compared with traditional fixed-wing and convertiplane, the short wing and strong lifting-wing multicopter rotor give it strong wind resistance..

History

In 2015, the University of Leuven, Belgium, proposed a hybrid configuration aircraft with a lifting-wing structure named VertiKUL2, whose wing and the rotor are installed at 45 degrees to improve wind resistance.

The reliable flight control group of Beihang University (rfly.buaa.edu.cn) formally proposed the lifting-wing multicopter configuration in 2018, and began the design and basic performance verification of the prototype of the lifting-wing multicopter. Compared with the traditional multicopter, it was concluded that the power consumption of the lifting-wing multicopter could be reduced by about 50% within a certain cruise speed range through experiments.

The prototype of the lifting-wing multicopter

In 2019, the reliable flight control group of Beihang University began the design of the lifting-wing multicopter, proposed evaluation methods for range and transition time performance and established a comprehensive model. Based on this, flight experiments were carried out, and the expected results were achieved.

The lifting-wing multicopter designed by the reliable flight control group of Beihang University

In 2019, VOLITATION designed a multicopter with a lifting wing named VesperTilio.

In the same year, Amazon designed Prime Air for delivery.

In 2022, the reliable flight control group of Beihang University carried out the unified controller verification experiments of lifting-wing multicopters and accurate trajectory tracking experiments

Characteristics

The lifting-wing multicopter is very different from the common hybrid UAV in control. It can smoothly transition from hovering to forward flight. During the forward flight, the rotors can provide the forward force and part of the lift of the UAV, while the lifting wing provides the other part of the lift. At the same time, the lifting wing's optimized design reduces the UAV's center of gravity, enhances stability, and avoids the danger of toppling due to the large windward surface when landing. Because of the advantages of the lifting-wing multicopter, its airframe design and flight control design are more complex than those of convertiplane and tail-sitter aircraft. Still, its use efficiency is significantly better than that of the latter.

Flight process of lifting-wing multicopters

Compared with the traditional multicopter, convertiplane, and tail-sitter aircraft, the lifting-wing multicopter has a relatively compromised performance, a supplement to the current hybrid UAV.

Performance comparison between the lifting-wing multicopter and other typical hybrid aircraft

Control

The reliable flight control group of Beihang University has designed a unified controller for the lifting-wing multicopter in the full flight stage, and rotors and ailerons on the lifting wing work together to save energy.

Unified control for full flight phases. Hybrid UAVs often have three different flight statuses, including the hover, the transition flight, and the forward flight. By taking the multicopter tilt-rotor/wing convertiplane, multicopter dual-system convertiplane, and multicopter tail-sitter example, their take-off and landing are controlled only by the quadcopter component, while the forward flight is controlled like a fixed-wing aircraft. The two control ways are very different, so the transition flight is challenging due to the nonlinearities and uncertainties. However, a full flight phase of the lifting-wing quadcopter always involves thrust by the quadcopter and aerodynamic force by the lifting wing. Therefore, the lifting-wing quadcopter can be considered under only the transition flight mode in the full flight phase (hover control here also will consider the aerodynamic force due to wind on the lifting wing). As a result, a unified control is needed. Fortunately, the lifting-wing quadcopter only needs to tilt a specific angle, often smaller than 45 degrees, rather than 90 degrees like tail sitter UAVs. This reduces the possibility of having a stall.

Cooperative control for energy saving. The transition flight for current hybrid UAVs is very short, so little attention must be paid to energy consumption in practice. However, it should be considered for the lifting-wing quadcopter as it is in transition flight mode in the full flight phase. Cooperative control for energy saving is feasible. For example, the lifting wing can perform roll control by both the quadcopter component and the ailerons. Obviously, the aileron control is more energy-saving.