The relative motion control for the unmanned quadrotors autonomous shipboard landings is investigated in this study. The shipboard
landing missions are divided into two phases including the position approaching phase and the vertical landing phase. Relative
pose kinematics and dynamics are modeled in the quadrotor’s body-fixed frame, where the kinematic couplings resulted from
the difference between ship’s centre of mass and desired landing site and the unknown external disturbances of two vehicles
are considered in the modeling and control design. In the position approaching phase, because of the under-actuated property of
quadrotors, the adaptive backstepping technique is combined with an auxiliary system and a command filter to develop the guidance
and control laws. Subsequently, the relative altitude-attitude controller is designed for the vertical landing phase. Stability analysis
shows that the position approaching errors in the first phase and the landing errors in the second phase ultimately converge to small
neighborhoods of zero, and numerical simulation validates the effectiveness of the proposed strategy.
Funding
National Natural Science Foundation of China [grant number 61903025]
China Scholarship Council [grant number 201906465028]
Beijing Natural Science Foundation [grant number 4202038]
Fundamental Research Funds for the Central Universities [grant numbers FRF-BD-19-002A, FRF-GF-18-0028B]
History
School
Aeronautical, Automotive, Chemical and Materials Engineering
This paper was accepted for publication in the journal Journal of the Franklin Institute and the definitive published version is available at https://doi.org/10.1016/j.jfranklin.2020.10.014