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May 25, 2026Journal of Vibration and Control0 citations

Real-time guidance and control for multi-fixed-wing unmanned aerial vehicles for standoff surveillance in cluttered environment

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MBMuhammad Imran BaigZZZiyang ZhenUJUmair Javaid

Key Points

  • This research aims to enhance the effectiveness of standoff surveillance operations using multiple fixed-wing UAVs in cluttered environments.
  • Proposed a blended guidance and flock control mechanism to unify vector field-based guidance and adaptive flock control.
  • Utilized Lyapunov stability theory to ensure convergence of flight paths of UAVs.
  • Conducted comparative numerical simulations and real-time hardware-in-loop tests to assess the proposed framework.
  • Numerical simulations showed improved obstacle avoidance and flocking behavior among multiple UAVs during surveillance.
  • Real-time HIL tests validated the effectiveness of the proposed BGFC framework for operational performance.
  • Optimization reduced energy consumption while maintaining surveillance path accuracy.

Abstract

The standoff surveillance operations (SSO) in a cluttered environment using multiple distributed fixed-wing unmanned aerial vehicle (FW-UAV)-based system present critical challenges. It requires real-time guidance for surveillance, obstacle avoidance in the flying path, and flock control. This study proposes a blended guidance and flock control (BGFC) mechanism that unifies the vector field-based hybrid guidance (VFHG) model and adaptive flock control (AFC) to address the SSO problem. Initially, the proposed VFHG model ensures that FW-UAVs follow the surveillance path while maintaining a safe distance from obstacles on the flying path within a finite time (FT). Later, the proposed AFC strategy ensures distributed flocking behavior in the multi-FW-UAV system during SSO. The dynamic nature of the FW-UAVs flock and adaptive interactions among system agents while maintaining safe clearance from each other are key features of the proposed AFC. Lyapunov stability theory is used to prove the convergence of the FW-UAV flight paths. In addition, an optimization problem is formulated to tune the design parameters of the proposed BGFC mechanism to achieve an optimal operational performance and minimize the energy consumption during the SSO. Comparative numerical simulations and real-time hardware-in-loop (HIL) tests confirm the efficiency of the proposed BGFC framework.

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Cite This Study

Baig et al. (2026) studied this question.

synapsesocial.com/papers/6a13e7cf0e02ee3982d3277chttps://doi.org/10.1177/10775463261449236
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