TY - GEN
T1 - A Model Predictive Control Integrated Framework for Quadrotor Robust Trajectory Tracking
AU - Hu, Kaikun
AU - Ye, Jianchuan
AU - Song, Tao
AU - Deng, Yixing
AU - Liu, Hao
N1 - Publisher Copyright:
© Press of Acta Aeronautica et Astronautica Sinica 2026.
PY - 2026
Y1 - 2026
N2 - This paper proposes an Model Predictive Control (MPC) integrated framework to enhance the trajectory tracking accuracy and robustness of quadrotor in dynamic environments. Addressing challenges in precision and disturbance rejection, the framework leverages a manifold-based MPC to directly optimize thrust and moments inputs while compensating for aerodynamic drag and external disturbances. By utilizing differential flatness for reference trajectory, the method formulates the control problem as a Quadratic Programming (QP) problem to compute optimal control increments. Simulations comparing the proposed framework with a baseline MPC-PID controller demonstrate significant improvements in tracking precision and robustness. The results validate that the control framework effectively balances computational efficiency with accurate control, enabling agile trajectory tracking even under external disturbances. This work advances the practical deployment of quadrotor in real world scenarios requiring agile and precise motion control.
AB - This paper proposes an Model Predictive Control (MPC) integrated framework to enhance the trajectory tracking accuracy and robustness of quadrotor in dynamic environments. Addressing challenges in precision and disturbance rejection, the framework leverages a manifold-based MPC to directly optimize thrust and moments inputs while compensating for aerodynamic drag and external disturbances. By utilizing differential flatness for reference trajectory, the method formulates the control problem as a Quadratic Programming (QP) problem to compute optimal control increments. Simulations comparing the proposed framework with a baseline MPC-PID controller demonstrate significant improvements in tracking precision and robustness. The results validate that the control framework effectively balances computational efficiency with accurate control, enabling agile trajectory tracking even under external disturbances. This work advances the practical deployment of quadrotor in real world scenarios requiring agile and precise motion control.
KW - Differential flatness
KW - Manifold-Based MPC
KW - Quadrotor
UR - https://www.scopus.com/pages/publications/105021810750
U2 - 10.1007/978-981-95-3010-6_41
DO - 10.1007/978-981-95-3010-6_41
M3 - Conference contribution
AN - SCOPUS:105021810750
SN - 9789819530090
T3 - Lecture Notes in Mechanical Engineering
SP - 601
EP - 612
BT - Proceedings of the 2nd Aerospace Frontiers Conference (AFC 2025) - Volume III
PB - Springer Science and Business Media Deutschland GmbH
T2 - 2nd Aerospace Frontiers Conference, AFC 2025
Y2 - 11 April 2025 through 14 April 2025
ER -