TY - JOUR
T1 - Robust helicopter sliding mode control for enhanced handling and trajectory following
AU - Halbe, Omkar
AU - Hajek, Manfred
N1 - Publisher Copyright:
© 2020 by Omkar Halbe. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
PY - 2020
Y1 - 2020
N2 - Helicopters in tactical missions require superior handling and stability in turbulence. This paper proposes a sliding mode control (SMC)-based helicopter trajectory controller for enhanced handling qualities (HQs) with robustness to endogenous (modeling) and exogenous (turbulence) uncertainties. The flight control problem is posed as one of attitude, angular rate, and translational rate command tracking with closed-loop axial responses conforming to predicted level 1 HQs. The required closed-loop behavior is then enforced by a two-loop output-tracking SMC treating interaxis coupling and turbulence as matched, bounded uncertainties. To mitigate the chattering effect of SMC, a continuous control approximation using the boundary-layer concept is applied. The stability and tracking performance of the two-loop controller are analyzed. Furthermore, actuator saturations encountered during aggressive maneuvers are mitigated by reference command adaptation based on pseudo-control hedging. The proposed controller is evaluated against selected HQ temporal response criteria, two mission task elements requiring moderate to aggressive agility, and a shipboard approach in high-intensity turbulence. Simulation results highlight the controller’s trajectory tracking accuracy, adequate axial decoupling, and insensitivity to disturbances.
AB - Helicopters in tactical missions require superior handling and stability in turbulence. This paper proposes a sliding mode control (SMC)-based helicopter trajectory controller for enhanced handling qualities (HQs) with robustness to endogenous (modeling) and exogenous (turbulence) uncertainties. The flight control problem is posed as one of attitude, angular rate, and translational rate command tracking with closed-loop axial responses conforming to predicted level 1 HQs. The required closed-loop behavior is then enforced by a two-loop output-tracking SMC treating interaxis coupling and turbulence as matched, bounded uncertainties. To mitigate the chattering effect of SMC, a continuous control approximation using the boundary-layer concept is applied. The stability and tracking performance of the two-loop controller are analyzed. Furthermore, actuator saturations encountered during aggressive maneuvers are mitigated by reference command adaptation based on pseudo-control hedging. The proposed controller is evaluated against selected HQ temporal response criteria, two mission task elements requiring moderate to aggressive agility, and a shipboard approach in high-intensity turbulence. Simulation results highlight the controller’s trajectory tracking accuracy, adequate axial decoupling, and insensitivity to disturbances.
UR - http://www.scopus.com/inward/record.url?scp=85090910571&partnerID=8YFLogxK
U2 - 10.2514/1.G005183
DO - 10.2514/1.G005183
M3 - Article
AN - SCOPUS:85090910571
SN - 0731-5090
VL - 43
SP - 1805
EP - 1821
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
IS - 10
ER -