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research-article

Platoon Control under a Novel Leader and Predecessor Following Scheme with the Use of an Advanced Aerodynamic Model

[+] Author and Article Information
Hakan Köroglu

Dept. Signals and Systems, Chalmers University of Technology, Gothenburg, Sweden, 41296
hakankoroglu@yahoo.com

Maryam Mirzaei

Dept. Applied Mechanics, Chalmers University of Technology, Gothenburg, Sweden, 41296
maryam.mirzaei@chalmers.se

Paolo Falcone

Dept. Signals and Systems, Chalmers University of Technology, Gothenburg, Sweden, 41296
paolo.falcone@chalmers.se

Sinisa Krajnovic

Dept. Applied Mechanics, Chalmers University of Technology, Gothenburg, Sweden, 41296
sinisa@chalmers.se

1Corresponding author.

ASME doi:10.1115/1.4037655 History: Received January 04, 2017; Revised August 11, 2017

Abstract

The longitudinal platoon control problem is considered under a leader and predecessor following scheme with a novel velocity-dependent spacing policy. With this spacing policy, the steady-state inter-vehicle distances increase with increasing cruise velocity and more so for vehicles that are closer to the leader.} Since significant changes might be encountered in inter-vehicle distances during the travel due to the variations in the velocity of the leader, the problem is studied together with a more accurate modeling of aerodynamic effects within a platoon formation. Based on a standard feedback linearization approach, a dynamic output feedback synthesis problem is formulated with two H_infinity performance objectives. One of the performance objectives is linked to the string stability of the platoon formation, while the other can be shaped in a way to maintain small spacing errors without aggressive vehicle maneuvers. A synthesis procedure is then outlined based on linear matrix inequality optimization. The new control scheme is investigated for a three-vehicle platoon by using an advanced aerodynamic model developed based on extensive fluid dynamics simulations. It is observed in this investigation that a desirable platoon operation can be achieved even with a simple aerodynamic model, provided that the controller is designed in a way to ensure good disturbance attenuation. Nevertheless an accurate modeling of aerodynamic disturbances might be needed especially for the first vehicle after the leader when the cruising velocity varies over a wide range.

Copyright (c) 2017 by ASME
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