Abstract
This paper proposes an analytical Koopman-based linear model predictive control (MPC) method for real-time quadrotor trajectory tracking. While linear MPC offers computational efficiency, it sacrifices modeling fidelity; nonlinear MPC solved via sequential quadratic programming achieves high accuracy but requires multiple iterations at each control step. We develop a systematic procedure to derive Koopman observables that lift the dynamics into a quasi-linear model with state-dependent control matrix. An assumed state trajectory converts this to a linear time-varying system at each control period, enabling quadratic program formulation with guaranteed real-time solvability. An incremental nonlinear dynamic inversion (INDI)-based robust control allocation scheme is proposed, which requires no precise control effectiveness model. Simulation results demonstrate tracking performance comparable to nonlinear MPC with deterministic computation times. The proposed method requires no training data collection, making it straightforward to implement.
| Original language | English |
|---|---|
| Title of host publication | 2026 IEEE 20th International Conference on Control and Automation (ICCA) : proceedings |
| Publisher | IEEE |
| Pages | 1086-1091 |
| Number of pages | 6 |
| DOIs | |
| Publication status | Published - Jun 2026 |
| Event | 2026 IEEE 20th International Conference on Control and Automation - Almaty, Kazakhstan Duration: 16 Jun 2026 → 19 Jun 2026 |
Publication series
| Name | IEEE International Conference on Control and Automation |
|---|---|
| Publisher | IEEE |
| ISSN (Print) | 1948-3449 |
| ISSN (Electronic) | 1948-3457 |
Conference
| Conference | 2026 IEEE 20th International Conference on Control and Automation |
|---|---|
| Abbreviated title | ICCA 2026 |
| Country/Territory | Kazakhstan |
| City | Almaty |
| Period | 16/06/26 → 19/06/26 |
Funding
This work was supported by the Postdoctoral Fellowship Program of CPSF under Grant Number “BX20240462”, the National Natural Science Foundation of China under Grants U2241217, 62373022, 62473029, 62403038, 62403238, and 62203032, the Beijing Natural Science Foundation under Grants JQ23019 and 4232046, and the Aeronautical Science Fund under Grant 2022Z071051015, 2023Z034051001.
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