Abstract

The operation of Unmanned Aerial Vehicles (UAVs) in civil airspace is restricted by the aviation authorities, which require full compliance with regulations that apply for manned aircraft. This paper proposes control algorithms for a collision avoidance system that can be used as an advisory system or a guidance system for UAVs that are flying in civil airspace under visual flight rules. A decision-making system for collision avoidance is developed based on the rules of the air. The proposed architecture of the decision-making system is engineered to be implementable in both manned aircraft and UAVs to perform different tasks ranging from collision detection to a safe avoidance manoeuvre initiation. Avoidance manoeuvres that are compliant with the rules of the air are proposed based on pilot suggestions for a subset of possible collision scenarios. The proposed avoidance manoeuvres are parameterized using a geometric approach. An optimal collision avoidance algorithm is developed for real-time local trajectory planning. Essentially, a finite-horizon optimal control problem is periodically solved in real-time hence updating the aircraft trajectory to avoid obstacles and track a predefined trajectory. The optimal control problem is formulated in output space, and parameterized by using B-splines. Then the optimal designed outputs are mapped into control inputs of the system by using the inverse dynamics of a fixed wing aircraft.

Highlights

  • Unmanned Aircraft Systems (UAS) are being increasingly used for both civilian and military applications due to their ability to complete dull, dirty and dangerous missions [1]

  • The proposed Decision-Making System (DMS) architecture is engineered to be implemented for different functionalities for manned aircraft, and at different level of autonomy of UAS, or at different classes of the flight control mode (Class-0 to Class-6) [46]

  • A multi-layer DMS is developed for a sense and avoid system based on the rules of the air in Visual Flight Rules (VFR) conditions

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Summary

Introduction

Unmanned Aircraft Systems (UAS) are being increasingly used for both civilian and military applications due to their ability to complete dull, dirty and dangerous missions [1]. The required time for a pilot to recognize an approaching aircraft and initiate an avoidance manoeuvre is around 12.5 s [6] but may be greater because pilots differ in their response time [7]. Most of this time is spent on collision recognition and decision making. A Decision-Making System (DMS) that could be used as an advisory system will effectively save time and help both the on-board pilot in manned aircraft, and the ground-based pilot for UAV’s to avoid the conflicts safely. In an autonomously operating UAV, a DMS could be used to initiate avoidance manoeuvres

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