The split flying car is composed of a flight module, a passenger capsule and an intelligent chassis module. The autonomous docking between these modules enables the split flying car to switch between flight mode and driving mode. The positioning of the aircraft bracket junction point is crucial for determining the desired position of the flight module. However, the complex and variable takeoff and landing environments and the limited computing power of edge computing platforms pose significant challenges to the perception task. To address these issues, we propose a lightweight network-based aircraft bracket detection model that meets real-time requirements in docking scenarios. Firstly, we use the inverse perspective mapping stitched bird's eye view as input to obtain the junction point coordinates of the aircraft bracket through the junction point detector. Then the position information of the bracket is obtained by eliminating the mis-detected junction points and reasoning out the missed junction points based on the a priori information of the aircraft bracket. To facilitate vision-based aircraft bracket detection research, a dataset is established, which is the first publicly available dataset in this research field, collecting 4,631 bird's eye views in different environments. The proposed method can achieve FPS of 35.79 and average precision of 0.915 in the Jetson AGX Xavier edge computing platform. The proposed method can also achieve competitive results when applied in parking slot detection with at least 2 ​× ​faster inference speed.

The hybrid electric propulsion system (HEPS) holds clear potential to support the goal of sustainability in the automobile and aviation industry. As an important part of the three-dimensional transportation network, vehicles and aircraft using HEPSs have the advantages of high fuel economy, low emission, and low noise. To fulfill these advantages, the design of their energy management strategies (EMSs) is essential. This paper presents an in-depth review of EMSs for hybrid electric vehicles (HEVs) and hybrid electric aircraft. First, in view of the main challenges of current EMSs of HEVs, the referenced research is reviewed according to the solutions facing real-time implementation problems, variable driving conditions adaptability problems, and multi-objective optimization problems, respectively. Second, the existing research on the EMSs for hybrid electric aircraft is summarized according to the hybrid electric propulsion architectures. In addition, with the advance in propulsion technology and mechanical manufacturing in recent years, flying cars have gradually become a reality, further enriching the composition of the three-dimensional transportation network. And EMSs also play an essential role in the efficient operation of flying cars driven by HEPSs. Therefore, in the last part of this paper, the development status of flying cars and their future prospects are elaborated. By comprehensively summarizing the EMSs of HEPS for vehicles and aircraft, this review aims to provide guidance for the research on the EMSs for flying cars driven by HEPS and serve as the basis for knowledge transfer of relevant researchers.

This research concerns a novel attitude stabilization structure for a ducted-fan aerial robot to work against modeling error and strong external transient disturbance, and it focuses on two main control targets: modeling error compensation, and the improvement of disturbance resistance along the rolling channel. For the first research objective, we proposed an adaptive nominal controller with the reconfigurable control law design based on the estimation of the modeling error found in the closed-loop. Results of simulations and corresponding flight tests verified that the proposed adaptive control structure is robust against both constant and time-varying modeling error. For the other research objective, a SAC (Stability Augmentation Control) structure was devised based on the CMG (Control Moment Gyroscope) theory in order to provide extra moment which effectively withstands the transient disturbance beyond the CDG (Critical Disturbance Gain). Furthermore, we studied the corresponding controller for the SAC via the SMC (sliding mode control) theory, while the working mechanism and performance of the SAC were verified through a specially devised prototype.