TY - GEN
T1 - Smooth Reference Command Generation and Control for Transition Flight of VTOL Aircraft Using Time-Varying Optimization
AU - Kim, Jinrae
AU - Bullock, John L.
AU - Cheng, Sheng
AU - Hovakimyan, Naira
N1 - This work is supported by NASA under the Cooperative Agreement 80NSSC20M0229 and University Leadership Initiative grant 80NSSC22M0070.
PY - 2025
Y1 - 2025
N2 - Vertical take-off and landing (VTOL) aircraft pose a challenge in generating reference commands during transition flight. While sparsity between hover and cruise flight modes can be promoted for effective transitions by formulating ℓ1-norm minimization problems, solving these problems offline pointwise in time can lead to non-smooth reference commands, resulting in abrupt transitions. This study addresses this limitation by proposing a time-varying optimization method that explicitly considers time dependence. By leveraging a prediction-correction interior- point time-varying optimization framework, the proposed method solves an ordinary differential equation to update reference commands continuously over time, enabling smooth reference command generation in real time. Numerical simulations with a two-dimensional Lift+Cruise vehicle validate the effectiveness of the proposed method, demonstrating its ability to generate smooth reference commands online.
AB - Vertical take-off and landing (VTOL) aircraft pose a challenge in generating reference commands during transition flight. While sparsity between hover and cruise flight modes can be promoted for effective transitions by formulating ℓ1-norm minimization problems, solving these problems offline pointwise in time can lead to non-smooth reference commands, resulting in abrupt transitions. This study addresses this limitation by proposing a time-varying optimization method that explicitly considers time dependence. By leveraging a prediction-correction interior- point time-varying optimization framework, the proposed method solves an ordinary differential equation to update reference commands continuously over time, enabling smooth reference command generation in real time. Numerical simulations with a two-dimensional Lift+Cruise vehicle validate the effectiveness of the proposed method, demonstrating its ability to generate smooth reference commands online.
UR - http://www.scopus.com/inward/record.url?scp=105001250577&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=105001250577&partnerID=8YFLogxK
U2 - 10.2514/6.2025-1123
DO - 10.2514/6.2025-1123
M3 - Conference contribution
AN - SCOPUS:105001250577
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 -