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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS

Modelling and characterisation of a rotary drive system with two opposing motors in the specific case of very low-speed movement AMOS SA

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Léonard, Noa ULiège
Promotor(s) : Salles, Loïc ULiège
Date of defense : 29-Jun-2026/30-Jun-2026 • Permalink : http://hdl.handle.net/2268.2/26097
Details
Title : Modelling and characterisation of a rotary drive system with two opposing motors in the specific case of very low-speed movement AMOS SA
Translated title : [fr] Modélisation et caractérisation d’un système d’entrainement rotatif avec deux moteurs en opposition dans le cas particulier d’un mouvement à très basse vitesse.
Author : Léonard, Noa ULiège
Date of defense  : 29-Jun-2026/30-Jun-2026
Advisor(s) : Salles, Loïc ULiège
Committee's member(s) : Collette, Christophe ULiège
Meant, Laurence 
Gabriel, Eric 
Language : English
Number of pages : 104
Keywords : [en] Dual-motor anti-backlash drive
[en] telescope azimuth axis control
[en] LuGre friction modelling
[en] cogging torque and gear-mesh disturbances
[en] system identification and PID control.
[en] low-speed accurate tracking
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Research unit : AMOS, Mechatronics Engineering
Target public : Researchers
Professionals of domain
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] This thesis investigates a dual-motor anti-backlash drive for the azimuth axis of ground-based telescopes operating at very low speed. The architecture relies on two opposing motor–gearbox assemblies acting on a common gear wheel: by applying an antagonistic preload, each motor suppresses the backlash of the other, improving tracking accuracy. A decommissioned polishing head was transformed into a dedicated test bench (2MOp); custom mechanical parts were designed and manufactured, and the electrical cabinet was rewired and fitted with a PLC. A modular Simulink model was developed, incorporating motor dynamics, LuGre friction, cogging torque, torque ripple, gear-mesh disturbances and encoder errors, and a PID position controller was tuned across trajectories ranging from steps to star and satellite tracking. The three-level control hierarchy (current, velocity, position) was then implemented on the bench, and the plant was identified by closed-loop white-noise injection. Experimental campaigns characterised the reduction ratios, friction parameters, gear-mesh frequencies and parasitic velocity oscillations. The two-stage gearbox of the second motor proved to generate disturbances large enough to prevent reliable dual-motor identification and tuning. With the first motor alone, the bench met its targets, achieving an RMS following error of 0.078 arcsec at sidereal speed and 2.14 arcsec at flip speed, the dominant residual disturbance being cogging torque.


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Author

  • Léonard, Noa ULiège Université de Liège > Master ing. civ. aéro., fin. spéc. aer. eng.

Promotor(s)

Committee's member(s)

  • Collette, Christophe ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Active aerospace struct. and adv. mecha. systems
    ORBi View his publications on ORBi
  • Meant, Laurence
  • Gabriel, Eric








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