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Vehicle System Dynamics
International Journal of Vehicle Mechanics and Mobility
Volume 62, 2024 - Issue 8
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Research Articles

Safe operating envelope based on a single-track model for yaw instability avoidance of articulated heavy vehicles

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Pages 2138-2161 | Received 10 Oct 2022, Accepted 23 Oct 2023, Published online: 16 Nov 2023

Figures & data

Figure 1. Illustrations of different yaw instabilities for a tractor (blue) and semitrailer (grey). (a) Jackknifing. (b) Trailer swing and (c) Combination spin-out.

Figure 1. Illustrations of different yaw instabilities for a tractor (blue) and semitrailer (grey). (a) Jackknifing. (b) Trailer swing and (c) Combination spin-out.

Figure 2. Free-body diagrams of the nonlinear single-track model for the AHV [Citation23,p.296]. Forces and moments are shown in blue, velocities in green.

Figure 2. Free-body diagrams of the nonlinear single-track model for the AHV [Citation23,p.296]. Forces and moments are shown in blue, velocities in green.

Figure 3. Paths followed by an AHV for two different braking manoeuvres with V1xinit=45 km/h, μ=0.3, R = 72 m. Braking starts at t=5s. (a) ctractor=0.8 and ctrailer=0. Jackknifing occurs and simulation is terminated when the articulation angle reaches 90 and (b) ctractor=0.75 and ctrailer=0.75. No yaw instability occurs and simulation is terminated when the tractor reaches zero velocity.

Figure 3. Paths followed by an AHV for two different braking manoeuvres with V1xinit=45 km/h, μ=0.3, R = 72 m. Braking starts at t=5s. (a) ctractor=−0.8 and ctrailer=0. Jackknifing occurs and simulation is terminated when the articulation angle reaches 90∘ and (b) ctractor=−0.75 and ctrailer=−0.75. No yaw instability occurs and simulation is terminated when the tractor reaches zero velocity.

Figure 4. Eigenvalues of the linearised single-track model, actuated with five different longitudinal force pairs. ctractor is the friction utilisation of the tractor's rear axle and ctrailer is the friction utilisation of the semitrailer's axle.

Figure 4. Eigenvalues of the linearised single-track model, actuated with five different longitudinal force pairs. ctractor is the friction utilisation of the tractor's rear axle and ctrailer is the friction utilisation of the semitrailer's axle.

Table 1. Eigenvalues of the nonlinear single-track model actuated with 13 different longitudinal force pairs.

Figure 5. AHV exhibiting a trailer swing due to semitrailer braking, with ctrailer=0.8 at t=5s.

Figure 5. AHV exhibiting a trailer swing due to semitrailer braking, with ctrailer=−0.8 at t=5s.

Figure 6. Changes in maximum articulation angle and side-slip angle deviations due to different values on the operational parameters: turning radius (first-row plots), initial speed (second-row plots), and friction coefficient (third-row plots) for three different braking manoeuvres. (a) [ctractorctrailer=0.80] (b) [ctractorctrailer=00.8] (c) [ctractorctrailer=0.80.8]

Figure 6. Changes in maximum articulation angle and side-slip angle deviations due to different values on the operational parameters: turning radius (first-row plots), initial speed (second-row plots), and friction coefficient (third-row plots) for three different braking manoeuvres. (a) [ctractorctrailer=−0.80] (b) [ctractorctrailer=0−0.8] (c) [ctractorctrailer=−0.8−0.8]

Figure 7. Effects of various friction utilisation ratios, ctractor and ctrailer. (a) ctractor[1,1] and ctrailer=0 and (b) ctractor=0 and ctrailer[1,1].

Figure 7. Effects of various friction utilisation ratios, ctractor and ctrailer. (a) ctractor∈[−1,1] and ctrailer=0 and (b) ctractor=0 and ctrailer∈[−1,1].

Figure 8. Maximum side-slip angle and articulation angle deviations for braking at six different speeds, according to the nonlinear single-track model.

Figure 8. Maximum side-slip angle and articulation angle deviations for braking at six different speeds, according to the nonlinear single-track model.

Figure 9. SOE obtained from the nonlinear single-track model of a braking AHV.

Figure 9. SOE obtained from the nonlinear single-track model of a braking AHV.

Figure 10. Different yaw instability modes shown on the SOE.

Figure 10. Different yaw instability modes shown on the SOE.

Figure 11. SOE obtained from the nonlinear single-track model of an accelerating AHV.

Figure 11. SOE obtained from the nonlinear single-track model of an accelerating AHV.

Figure 12. Slice of the SOE obtained from the nonlinear single-track model for 40 km/h (cy=0.561) for any combination of propulsion and braking forces.

Figure 12. Slice of the SOE obtained from the nonlinear single-track model for 40 km/h (cy=0.561) for any combination of propulsion and braking forces.