ORIGINAL RESEARCH

Aerosp. Res. Commun.

A Minimum Snap Flight Transition Strategy for Quadrotor Tail-sitter UAVs: Altitude-hold Transition

  • Zhejiang University, Hangzhou, China

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Abstract

This paper studies the altitude-hold flight mode transition problem for tail-sitter unmanned aerial vehicles (UAVs) between hovering and level flight. The problem is significantly challenging because of the complicated nonlinear aerodynamics of the tail-sitter UAV during the transition process. This paper proposes a minimum snap trajectory generation method and a model predictive control (MPC) based tracking strategy for this problem. Firstly, the generated trajectory are highly applicable, satisfying the dynamic constraint. Secondly, MPC tracks full states by solving a finite-horizon optimization at each step to yield the best future behavior based on the system model. A numerical simulation is conducted, in which the altitude change is less than 1.4 m during the entire transition process.

Summary

Keywords

Autonomous aerial vehicles, altitude-hold transition, vehicle dynamics, flight mode transition control, tail-sitter UAVs

Received

21 August 2025

Accepted

06 November 2025

Copyright

© 2025 Fan and Xia. This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) or licensor are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.

*Correspondence: Yifan Xia, xiayifan@zju.edu.cn

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