Výsledky vyhledávání - "optimal control allocation algorithm"

Development of a Full Orientation Flight Robotics: Dynamics Modeling, Analysis, and Control Design Autor Li, Yang-Rui, Peng, Chao-Chung

“… Owing to the existence of the multi-rotor-driving redundancy, the optimal control allocation algorithm is further proposed to address the inverse mapping problem between the control signal channels…”
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Online Active Fault Detection for Over-Actuated Systems With Prescribed Control Performance Autor Cao, Fangfei, He, Xiao

“…In the field of fault detection, active fault detection for dynamic systems is an emerging research topic. By redesigning the control input, active fault…”
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Optimal Control Allocation-Based Automatic Transmission Upshift Control Strategy for Inertia Phase Autor Cvok, Ivan, Deur, Josko, Ivanovic, Vladimir, Zhang, Yijing, Fujii, Yuji

“… for faster product development. The strategy consists of a static model-based predictive controller coupled with an optimal control allocation algorithm…”
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Active vibration suppression for flexible satellites using a novel component synthesis method Autor Zhang, Liang, Xu, Shijie, Zhang, Zhiping, Cui, Naigang

“…This paper is devoted to developing a closed-loop vibration suppression controller for a satellite with large flexible appendages based on component synthesis…”
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On the control allocation of fully actuated multirotor aerial vehicles Autor Santos, Davi A., Bezerra, José A.

“…The present work deals with the optimal control allocation of fully actuated multirotor aerial vehicles (MAVs) equipped with fixed (non-vectoring and…”
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Integrated Control of Differential Braking and Active Aerodynamic Control for Improving High Speed Stability of Vehicles Autor Chen, Zhengqiang, Wu, Yiwan, Li, Fan

“…In this paper, an integrated control strategy (ICS) is proposed to improve high speed dynamics stability of the vehicle by the integration of active…”
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Tailless aircraft flight control using multiple time scale reconfigurable sliding modes Autor Shtessel, Y., Buffington, J., Banda, S.

“… An optimal control allocation algorithm is employed using nominal mathematical model of an aircraft…”
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Coordinated Chassis Control of 4WD Vehicles Utilizing Differential Braking, Traction Distribution and Active Front Steering Autor Feng, Jianbo, Chen, Sizhong, Qi, Zhiquan

“… intention and the consideration of vehicle stability, and the control allocation layer to distribute the actual control inputs to the actuators applying an optimal control allocation algorithm…”
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Vehicle High Speed Stability Analysis throughIntegrated Control Autor Nadhiya, Nur Alyani, Yakub, Fitri, Ariff, Hatta, Azizan, Azizul, Rasit, Zainuddin A., Ahmad Zaki, Sheikh, Abd Fattah, Abdul Yasser, Mori, Yasuchika

“…This paper extends the analysis of Yakub et. al [1], by suggesting an integrated control which includes an active aerodynamic control and differential braking…”
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Steering stability control for the four in-wheel motor independent-drive vehicle based on the optimal control Autor Haonan Peng, Wei Zhang, Weida Wang, Changle Xiang, Xunming Li

“… A hierarchical steering stability control strategy based on the LQR optimal control and the optimal control allocation algorithm is proposed in this paper…”
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Investigation of Optimal Control Allocation for Gust Load Alleviation in Flight Control Autor Frost, Susan A, Taylor, Brian R, Bodson, Marc

“…Advances in sensors and avionics computation power suggest real-time structural load measurements could be used in flight control systems for improved safety…”
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Nonlinear vehicle dynamics control for EV with 4 in-wheel motors Autor Xiong, Lu, Yu, Zhuoping, Meng, Yufeng

“…) theory was designed. Combining the controller with optimal control allocation algorithm which takes into account of longitudinal/lateral force couple characteristic for tire under critical situation, we designed…”
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Nonlinear disturbance observer-based finite-time convergent second order sliding mode control for a tailless aircraft Autor Li Peng, Qin Wei-wei, Zheng Zhi-qiang

“… An optimal control allocation algorithm is employed using nominal mathematical model of an aircraft…”
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