Yang Zhao

Dr. Yang Zhao

orcid

Research Focus & Metrics

Academic Career Length

1Year (2026-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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16 July 2026 in Drones
Verified
Journal Article
Open access
PDF file
YZYang Zhao
Yang Zhao
MHMingying Huo
Mingying Huo
NQNaiming Qi
Naiming Qi
LWLiguang Wang
Liguang Wang
ZXZongquan Xia
Zongquan Xia
GYGe Yang
Ge Yang
Challenges in trajectory planning are encountered by fixed-wing unmanned aerial vehicle (UAV) swarms operating in environments with unknown obstacles. In this study, a distributed real-time trajectory-planning method that integrates a distributed model predictive control (DMPC) framework with an adaptive Gaussian collocation strategy (DA-GCMPC) was developed. This method leverages a distributed iterative computational framework based on DMPC to reformulate trajectory planning as an optimal control problem. To address the fixed-resolution limitation of conventional distributed MPC formulations, a complexity-aware adaptive collocation mechanism is introduced. The novelty of the method lies in adapting the collocation transcription resolution of each local MPC problem according to the instantaneous planning complexity. This mechanism selects the collocation type online according to maneuvering demand, obstacle density risk, and neighboring-UAV interaction risk, enabling the planner to balance real-time computation and constraint-handling capability under limited perception. We decomposed the UAV energy consumption and formulated the total energy consumption of the swarm as the objective function. An optimal control sequence was derived using the Gaussian collocation method by integrating obstacle avoidance constraints for fixed-wing UAVs and environmental limitations. Comparative simulations against the implemented fixed-discretization interior-point and SQP baselines showed that the proposed DA-GCMPC method achieved lower computation time and better trajectory quality metrics under the tested simulation settings, with average per-step computation times below 80 ms. In addition, an eight-UAV semi-physical hardware-in-the-loop validation was conducted to verify the real-time executability of the proposed method in a closed-loop flight control system.

6 August 2026 in Aerospace Science and Technology
Verified
Journal Article
Closed access
YXYingdong Xia
Yingdong Xia
YZYang Zhao
Yang Zhao
YWYeguang Wang
Yeguang Wang
SWShipeng Wang
Shipeng Wang
BQBo Qi
Bo Qi
MHMingying Huo
Mingying Huo