TY - GEN
T1 - Autotuning the Unified Control and Generalized Control Allocation for VTOL Vehicles using DiffTune
AU - Kim, Minkyung
AU - Cheng, Sheng
AU - Hovakimyan, Naira
N1 - This work is supported by NASA under the Cooperative Agreement 80NSSC20M0229 and University Leadership Initiative grant 80NSSC22M0070, NSF-AoF Robust Intelligence award #2133656, and NSF SLES #2331878. We acknowledge the Intelligent Contingency Management group at NASA Langley Research Center for developing the original GUAM simulator and insightful discussions.
PY - 2025
Y1 - 2025
N2 - Vertical takeoff and landing (VTOL) vehicles are gaining attention in advanced air mobility (AAM) because of their versatility and efficiency. Transitioning VTOL vehicles are designed to transition between different flight modes, where mode-specific control approaches are commonly used. Recently, a unified control design is proposed to utilize a single control structure across the entire flight envelope. While this approach has the advantage of control uniformity and simplicity in control implementation, the control parameters still need to be tuned jointly for a unified performance metric regarding the vehicle’s flight. Yet, the high dimensionality of the parameter space and the non-linearity of the cascaded control and allocation make tuning by hand challenging and demand more efficient tools to reduce the tuning effort and improve tuning quality than a trial-and-error type of manual tuning. DiffTune is a gradient-based autotuning method that can effectively tune high-dimensional nonlinear systems. In this study, we use DiffTune for the unified control design and generalized control allocation to automate the control tuning of VTOL vehicles. We leverage the Lift+Cruise vehicle in the Generic Urban Air Mobility (GUAM) simulator and demonstrate the efficiency and effectiveness of the proposed method compared with the state-of-the-art autotuning method. DiffTune achieves nearly minimal tracking error after the first iteration and reduces the tracking error by up to 87.5% compared to the average of the minimum error obtained by the baseline method.
AB - Vertical takeoff and landing (VTOL) vehicles are gaining attention in advanced air mobility (AAM) because of their versatility and efficiency. Transitioning VTOL vehicles are designed to transition between different flight modes, where mode-specific control approaches are commonly used. Recently, a unified control design is proposed to utilize a single control structure across the entire flight envelope. While this approach has the advantage of control uniformity and simplicity in control implementation, the control parameters still need to be tuned jointly for a unified performance metric regarding the vehicle’s flight. Yet, the high dimensionality of the parameter space and the non-linearity of the cascaded control and allocation make tuning by hand challenging and demand more efficient tools to reduce the tuning effort and improve tuning quality than a trial-and-error type of manual tuning. DiffTune is a gradient-based autotuning method that can effectively tune high-dimensional nonlinear systems. In this study, we use DiffTune for the unified control design and generalized control allocation to automate the control tuning of VTOL vehicles. We leverage the Lift+Cruise vehicle in the Generic Urban Air Mobility (GUAM) simulator and demonstrate the efficiency and effectiveness of the proposed method compared with the state-of-the-art autotuning method. DiffTune achieves nearly minimal tracking error after the first iteration and reduces the tracking error by up to 87.5% compared to the average of the minimum error obtained by the baseline method.
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U2 - 10.2514/6.2025-1122
DO - 10.2514/6.2025-1122
M3 - Conference contribution
AN - SCOPUS:105001392783
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -