Abstract
Over the next decade, the growth of commercial aircraft is expected to increase by 30%, causing significant challenges in air traffic management and control. To address this problem, we propose the idea of aircraft platooning during the descending and pre-landing phases. The objective is to design a distributed flight guidance and control system that assists onboard pilots in finding a feasible and collision-free trajectory from descent to pre-landing. The proposed aircraft platoon control scheme comprises a feedback linearising controller in the inner loop that transforms the nonlinear aircraft dynamics into a MIMO double-integrator, inherently a Negative Imaginary system. The outer loop employs a distributed output feedback Strictly Negative Imaginary controller, enabling networked aeroplanes to maintain the desired inter-aircraft spacing along each coordinate by synchronising their velocities. In addition, a contingency strategy is proposed to handle potential runway failures (e.g. sudden blockage, damage, etc.) by switching a descending aircraft platoon into a time-varying hover formation for each aircraft, maintaining a safe vertical gap. Finally, a comprehensive MATLAB simulation case study is conducted to test the feasibility and performance of the NI theory-based aircraft platoon control scheme.
Original language | English |
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Title of host publication | Proceedings of the 22nd European Control Conference, Stockholm, Sweden, Jun 2024 |
DOIs | |
Publication status | Published - 24 Jul 2024 |
Event | Proceedings of the 22nd European Control Conference, Stockholm, Sweden, Jun 2024 - Stockholm, Sweden Duration: 25 Jun 2024 → 28 Jun 2024 |
Conference
Conference | Proceedings of the 22nd European Control Conference, Stockholm, Sweden, Jun 2024 |
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Country/Territory | Sweden |
City | Stockholm |
Period | 25/06/24 → 28/06/24 |