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Koopman-Based Linear MPC with INDI for Quadrotor Trajectory Tracking Control

  • Xiaokang LÜ
  • , Qing WANG*
  • , Shimin WANG
  • , Xiwang DONG
  • *Corresponding author for this work

Research output: Book Chapters | Papers in Conference ProceedingsConference paper (refereed)Referred Conference Paperpeer-review

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 languageEnglish
Title of host publication2026 IEEE 20th International Conference on Control and Automation (ICCA) : proceedings
PublisherIEEE
Pages1086-1091
Number of pages6
DOIs
Publication statusPublished - Jun 2026
Event2026 IEEE 20th International Conference on Control and Automation - Almaty, Kazakhstan
Duration: 16 Jun 202619 Jun 2026

Publication series

NameIEEE International Conference on Control and Automation
PublisherIEEE
ISSN (Print)1948-3449
ISSN (Electronic)1948-3457

Conference

Conference2026 IEEE 20th International Conference on Control and Automation
Abbreviated titleICCA 2026
Country/TerritoryKazakhstan
CityAlmaty
Period16/06/2619/06/26

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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