Abstract

The key to the integration of unmanned aircrafts in the national airspace is to prevent them from colliding with the other traffics in the airspace. However, it is a great challenge to generate a safe, stable and robust collision-free path for unmanned aircraft system (UAS), a.k.a. unmanned aircraft vehicle (UAV), in real time, if the airspace is highly dynamics and heterogenous (i.e. thronged with aircrafts with different motion states). Based on the dynamic artificial potential field (DAPF) algorithm, this paper provides advisories on how to generate a real-time reactive collision-free path for unmanned aircraft vehicles flying in a dynamic airspace, aiming to ensure the flight safety and minimize the impact on surrounding traffic. Firstly, the safety distance was defined as a variable threshold, which scaled adaptively according to the relative motion states of the surrounding obstacles and the performance of the own UAV. Moreover, the forces of the potential field were improved, such that their magnitudes could be adjusted automatically according to the threat levels of the surrounding obstacles. The threat level of an obstacle depends on the relative position, speed and flight trend between the UAV and the obstacle. In addition, the repulsive force along the relative position of the traditional artificial potential field (APF) was retained, and a steering force was added to change the flight direction of the UAV, aiming to speed up the collision avoidance. Furthermore, the attractive force was modified to help the UAV return to the planned path quickly and stably. After that, the capacity were determined to ensure the feasible and practical path planning for the UAV. Finally, the proposed UAV path-planning method was proved effective, safe, stable and adaptive through simulations.

Highlights

  • The last decade witnessed rapid development of unmanned aircraft system (UAS), a.k.a. unmanned aircraft vehicle (UAV)

  • I where, Uatt and Urep are the potential field functions of the attractive force and the repulsive force, respectively; Fatt and Frep are the attractive force and the repulsive force, respectively; Ftotal is the resultant force; i is the number of obstacles; kα and kβ are the proportional gains of the attractive force and the repulsive force, respectively; pg is the position of the destination; p is the position of the robot; d is the actual distance between the obstacle and the robot; rsafe is the safety distance threshold

  • FLYABILITY VERIFICATION OF COLLISION-FREE PATHS Figure 12 shows the variations in speed, acceleration and turning rate of artificial potential field (APF) and dynamic artificial potential field (DAPF) in the encounter scenes mentioned in Section B, and compares the two methods in the maximum speed, maximum acceleration and maximum turning rate

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Summary

INTRODUCTION

The last decade witnessed rapid development of unmanned aircraft system (UAS), a.k.a. unmanned aircraft vehicle (UAV). Based on the APF and the bacterial evolution method, Oscar Montiel et al [23] put forward a path planning approach to prevent collision between moving and static obstacles in a complex, dynamic environment, which can determine the optimal paths in a flexible and efficient manner. The relevant studies mostly tackle the inherent defects of the traditional targets, such as unreachability, local oscillation and path non-flyability When it comes to the real-time collision avoidance against moving obstacle, the existing APF methods often views moving obstacle as instantaneous static, and ignores the motion state and flying trend of the obstacle in each step. The traditional APF methods cannot effectively achieve the real-time collision avoidance of the UAV in a dynamic airspace with different obstacles. The remainder of this paper is organized as follows: Section II formulates the problem and describes the kinematics model of the UAV; Section III introduces the DAPF collision-free path generation method; Section IV verifies and analyzes the performance of our algorithm from different perspectives; Section V puts forward the conclusions

PROBLEM STATEMENT
TRADITIONAL APF
IMPROVEMENT OF ARTIFICIAL POTENTIAL FIELD METHOD
SIMULATION EXPERIMENT
CONCLUSION
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