scholarly journals A Robotic Head Stabilization Device for Medical Transport

Robotics ◽  
2019 ◽  
Vol 8 (1) ◽  
pp. 23
Author(s):  
Adam Williams ◽  
Bijo Sebastian ◽  
Pinhas Ben-Tzvi

In this paper, the design and control of a robotic device intended to stabilize the head and neck of a trauma patient during transport are presented. When transporting a patient who has suffered a traumatic head injury, the first action performed by paramedics is typically to restrain and stabilize the head and cervical spine of a patient. The proposed device would drastically reduce the time required to perform this action while also freeing a first responder to perform other possibly lifesaving actions. The applications for robotic casualty extraction are additionally explored. The design and construction are described, followed by control simulations demonstrating the improved behavior of the chosen controller paradigm, linear active disturbance rejection control (LADRC). Finally, experimental validation is presented, followed by future work and directions for the research.

Author(s):  
Bo Li ◽  
Wenqing Ge ◽  
Xiao Yu ◽  
Shilei Shao ◽  
Haitao Liu

Automated mechanical transmission has many advantages such as simple structure, high mechanical efficiency, and low cost. But the poor gearshift performance restricts the massive application of the automated mechanical transmission, and it can be improved through innovation of structure and control. To reduce the requirement of shift force and improve the shift performance, a new direct-drive electromagnetic gearshift system which consists of servo synchronizer and 2-degree-of-freedom electromagnetic actuator is adopted. The specific structure and working principle of the gearshift system including servo synchronizer are described, and the equation of force-amplifying ratio is deduced. Due to the complexity of the gearshift system and uncertainties of the gearshift process, active disturbance rejection control method is designed. The active disturbance rejection controller can eliminate the nonlinearity of the 2-degree-of-freedom actuator. The extended state observer can estimate and compensate the uncertainties, parameter variations, and external disturbances. Simulations are carried out, and the result comparison with proportional–integral–derivative controller indicates the superiority of the active disturbance rejection control method. Test bench and control system are developed to verify the performance of the newly designed system and control method. The experimental results show that, when the gearshift system is equipped with servo synchronizer, the driving force and the maximum volatility of driving force can be reduced by 35% and 5%, respectively, and the impact generated by active disturbance rejection control method is reduced by 36% compared with proportional–integral–derivative method. The new gearshift system achieves a better gearshift performance. Combined with the newly designed control strategy, the direct-drive electromagnetic gearshift system provides a new solution for automated mechanical transmission applications.


Author(s):  
Cong Zhang ◽  
Yun-Jie Wu

This paper proposes a novel integrated guidance and control (IGC) method combining dynamic surface control (DSC) and active disturbance rejection control (ADRC) for the guidance and control system of hypersonic reentry missile (HRM) with bounded uncertainties. First, the model of HRM is established. Second, the proposed IGC method based on DSC and ADRC is designed. The stability of closed-loop system is proved strictly. It is worth mentioning that the ADRC technique is used to estimate and compensate the disturbance in the proposed IGC system. This makes the closed-loop system a better performance and reduces the chattering caused by lumped disturbances. Finally, a series of simulations and comparisons with a 6-DOF non-linear missile that includes all aerodynamic effects are demonstrated to illustrate the effectiveness and advantage of the proposed IGC method.


Author(s):  
Juan Diaz-Tellez ◽  
Jaime Estevez-Carreón ◽  
Alejandro Silva-Juárez ◽  
Rubén Senén García-Ramírez

This paper proposes a robust attitude tracking control applied to Vertical Take-off and Landing Micro Aerial Vehicles (VANT) based on Active Disturbance Rejection Control (ADRC) approach. The proposed technique groups the endogenous and exogenous disturbances into a total disturbance, which is estimated online via extended state observer (ESO). Once the disturbance is determined, a quaternion-based controller is proposed, which compensates and relieves the disturbance actively. The control law is bounded; consequently, it takes into account the maximum capabilities of the actuators. The stability proof of the closed-loop (observer and control) is guaranteed in the ISS sense. The simulation results allow validating the theoretical features.


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