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Relevant bibliographies by topics / Sliding mode control Measured thrust

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Academic literature on the topic 'Sliding mode control Measured thrust'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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Journal articles on the topic "Sliding mode control Measured thrust"

1

Lin, Faa-Jeng, Syuan-Yi Chen, and Ming-Shi Huang. "Adaptive complementary sliding-mode control for thrust active magnetic bearing system." Control Engineering Practice 19, no. 7 (2011): 711–22. http://dx.doi.org/10.1016/j.conengprac.2011.03.006.

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Liu, Hui, Junfeng Li, and Baoyin Hexi. "Sliding mode control for low-thrust Earth-orbiting spacecraft formation maneuvering." Aerospace Science and Technology 10, no. 7 (2006): 636–43. http://dx.doi.org/10.1016/j.ast.2006.04.008.

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Derbel, Khaoula, and Károly Beneda. "Sliding Mode Control for Micro Turbojet Engine Using Turbofan Power Ratio as Control Law." Energies 13, no. 18 (2020): 4841. http://dx.doi.org/10.3390/en13184841.

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The interest in turbojet engines was emerging in the past years due to their simplicity. The purpose of this article is to investigate sliding mode control (SMC) for a micro turbojet engine based on an unconventional compound thermodynamic parameter called Turbofan Power Ratio (TPR) and prove its advantage over traditional linear methods and thrust parameters. Based on previous research by the authors, TPR can be applied to single stream turbojet engines as it varies proportionally to thrust, thus it is suitable as control law. The turbojet is modeled by a linear, parameter-varying structure, and variable structure sliding mode control has been selected to control the system, as it offers excellent disturbance rejection and provides robustness against discrepancies between mathematical model and real plant as well. Both model and control system have been created in MATLAB® Simulink®, data from real measurement have been taken to evaluate control system performance. The same assessment is conducted with conventional Proportional-Integral-Derivative (PID) controllers and showed the superiority of SMC, furthermore TPR computation using turbine discharge temperature was proven. Based on the results of the simulation, a controller layout is proposed and its feasibility is investigated. The utilization of TPR results in more accurate thrust output, meanwhile it allows better insight into the thermodynamic process of the engine, hence it carries an additional diagnostic possibility.

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Mishra, Amardeep. "Autonomous obstacle avoidance maneuvering of thrust-vectored airship with neural network control." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234, no. 3 (2019): 689–708. http://dx.doi.org/10.1177/0954410019879821.

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There has been a renewed interest in recent times in airship technology owing to its potential usage for applications ranging from defense, scientific exploration, advertising to even remote monitoring. For airships to expand operational profile, further enhancement of configurational features and control development for full autonomy are key technologies gaining attention. In this paper, beginning with the mathematical modeling of a thrust-vectored airship, the integrated motion planning and controller development for vehicle autonomy, taking into account various uncertainties, are dealt with. A rapidly exploring random tree-based obstacle avoidance path planning exercise is carried out to chart out a trajectory in the presence of obstacles. Then, a neural network-based sliding mode controller is subsequently designed that learns the unknown equivalent control in sliding mode control framework to track the reference trajectory. Simulation results presented at the end demonstrate the effectiveness of the approach.

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Feng, Chieh Chuan, Li Peng Yin, and En Chih Chang. "Robust Control Design Based-On Integral Sliding-Mode Control." Applied Mechanics and Materials 284-287 (January 2013): 2301–4. http://dx.doi.org/10.4028/www.scientific.net/amm.284-287.2301.

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This paper proposes a robust control design based-on integral sliding-mode and H2–norm performance criterion to handle a class of time-varying systems with perturbations including non-linearities and disturbances. The stabilization problems for such systems are studied: integral slid-ing-mode is designated to completely nullify the matched perturbations and, in the meantime, elim-inate the reaching phase to the sliding surface, while H2–norm is a robust linear control measured for system on the sliding surface. In addition to the integral sliding mode control, the contribution of the paper is to implement a parameter-dependent Lyapunov function for H2–norm robust linear control that the overall designed system is less conservative for the system with both matched and unmatched perturbations.

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Li, Bingqian, Wenhan Dong, and Xiaoshan Ma. "Backstepping Fault-Tolerant Control for Unmanned Thrust-Vectoring Aircraft Based on Sliding-Mode Observer." Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 36, no. 5 (2018): 978–87. http://dx.doi.org/10.1051/jnwpu/20183650978.

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In this paper, a backstepping fault-tolerant control based on sliding-mode observer is proposed for the unmanned thrust-vectoring aircraft (UTVA) control. First, the UTVA model with the uncertainty, control surface damage and actuator faults is described, which is divided into fast loop and slow loop. Next, the cascade observers including a high-order SMO and the discontinuous projection adaptive law are proposed to estimate the states with compensating the uncertainty and control surface damage, and the sliding-mode observer is designed to identify actuator faults and estimate fault parameters. Then, the backstepping fault-tolerant control combining the estimation of states and fault parameters is proposed to achieve the global fault-tolerant control, which compensates the uncertainty, control surface damage and actuator faults. Finally, simulation results are given to demonstrate the effectiveness for UTVA.

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Zhao, Lin, Kun Zhao, Hui Li, Weiquan Huang, Xinyu Zhang, and Xiangxi Zeng. "Loosely displaced formation-keeping control for satellite swarm with continuous low-thrust." International Journal of Advanced Robotic Systems 17, no. 5 (2020): 172988142094755. http://dx.doi.org/10.1177/1729881420947558.

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Aiming at a long-term formation-keeping problem for the satellite swarm, the concept of a loosely displaced formation is proposed in this article. On this basis, a continuous low-thrust control strategy for maintaining the loosely displaced formation is designed. The control objective is to reduce more fuel consumption during the formation-keeping. For achieving that, we proposed a forward-feedback control strategy by using pseudo-spectral method and sliding mode theory. To be specific, the control strategy includes two parts: a forward control and a feedback control. For the forward control, a numerical optimization with the Legendre pseudo-spectral method is attempted to convert the optimal control problem into a nonlinear programming problem and fuel consumption is selected as the optimization index. For stability issue, the feedback control via adaptive finite-time sliding mode theory is introduced as an additional control component. Finally, the numerical results demonstrate that propellant mass is effectively saved as well as the formation can be tracked accurately with this control strategy proposed in this article.

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Yeh, F. K. "Adaptive-sliding-mode guidance law design for missiles with thrust vector control and divert control system." IET Control Theory & Applications 6, no. 4 (2012): 552. http://dx.doi.org/10.1049/iet-cta.2011.0227.

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Bai, Jie, Shuai Liu, and Wang Wei. "The Nonlinear Single Controller of DGEN380 Aero Engine Design." International Journal of Aerospace Engineering 2019 (July 2, 2019): 1–12. http://dx.doi.org/10.1155/2019/7209428.

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The advanced nonlinear sliding mode control method of DGEN380 aero engine is presented in this paper. This aero engine is a small high bypass ratio turbofan engine by which the nonlinear control approach of the aero engine is invested. And this paper focuses on the power management function of the aero engine control system which includes steady control and transient control. The mathematical model of DGEN380 aero engine is built by a set of nonlinear dynamic equation that is validated by experimental data. The single controller based on sliding mode approach is designed that can keep some certain thrust levels during steady state and maintain repeatable performance during transient operation from one requested thrust level to another. The single controller can offset the impact of the signal noise and harmonic disturbance at a certain power point. And the dynamic performance of the single controller is satisfactory at the transient process. The experiment is conducted by aero engine test bench for the single control.

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Yang, Bo, Jun Miao, and Yong Yang. "Terminal Sliding Mode Control of a Lunar Lander with Electric Propulsion." Applied Mechanics and Materials 494-495 (February 2014): 1195–201. http://dx.doi.org/10.4028/www.scientific.net/amm.494-495.1195.

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This paper presents an attitude control method based on electric propulsion systems for the lunar lander that considers the important characteristics of nonlinearity and uncertainty of lunar soft landing maneuvers with large attitudes. The attitude control law is designed according to the terminal sliding mode variable structure control method. A soft lunar landing utilizing the proposed control method is simulated, and the results show that this attitude control system demonstrates superior global robustness, consumes less propellant, and can achieve higher precision than a conventional chemical propulsion-based control system. For a lunar lander with a pulse plasma thruster as the propulsion system, the attitude control precision of the system is 0.002 degrees when the attitude control force is 0.1 Newtons. When a conventional chemical, not electric, propulsion thruster is used, if the attitude control force decreases by one order of magnitude, then the control precision of the lunar lander decreases 10-fold. This study demonstrates that a terminal sliding mode variable structure control method combined with low level thrust electric propulsion can improve the precision of lunar soft landings.

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Dissertations / Theses on the topic "Sliding mode control Measured thrust"

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Jebelli, Ali. "Development of Sensors and Microcontrollers for Underwater Robots." Thesis, Université d'Ottawa / University of Ottawa, 2014. http://hdl.handle.net/10393/31283.

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Nowadays, small autonomous underwater robots are strongly preferred for remote exploration of unknown and unstructured environments. Such robots allow the exploration and monitoring of underwater environments where a long term underwater presence is required to cover a large area. Furthermore, reducing the robot size, embedding electrical board inside and reducing cost are some of the challenges designers of autonomous underwater robots are facing. As a key device for reliable operation-decision process of autonomous underwater robots, a relatively fast and cost effective controller based on Fuzzy logic and proportional-integral-derivative method is proposed in this thesis. It efficiently models nonlinear system behaviors largely present in robot operation and for which mathematical models are difficult to obtain. To evaluate its response, the fault finding test approach was applied and the response of each task of the robot depicted under different operating conditions. The robot performance while combining all control programs and including sensors was also investigated while the number of program codes and inputs were increased.

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Book chapters on the topic "Sliding mode control Measured thrust"

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Cheema, Muhammad Ali Masood, and John Edward Fletcher. "Sensorless Control of a Linear Permanent Magnet Synchronous Motors Using a Combined Sliding Mode Adaptive Observer." In Advanced Direct Thrust Force Control of Linear Permanent Magnet Synchronous Motor. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-40325-6_7.

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Liu, Junjie, Zengqiang Chen, Mingwei Sun, and Qinglin Sun. "High Angle of Attack Sliding Mode Control for Aircraft with Thrust Vector Based on ESO." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-32-9682-4_6.

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Piao, Zaiji, and Chen Guo. "Research on Sliding Mode Active Disturbance Rejection Control and Thrust Allocation of Dynamic Positioning System." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-32-9050-1_30.

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Cheema, Muhammad Ali Masood, and John Edward Fletcher. "Sliding Mode Based Combined Speed and Direct Thrust Force Control of a Linear Permanent Magnet Synchronous Motors." In Advanced Direct Thrust Force Control of Linear Permanent Magnet Synchronous Motor. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-40325-6_6.

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Conference papers on the topic "Sliding mode control Measured thrust"

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Fu-Kuang Yeh, Hsiuan-Hau Chien, and Li-Chen Fu. "Nonlinear optimal sliding mode midcourse controller with thrust vector control." In Proceedings of 2002 American Control Conference. IEEE, 2002. http://dx.doi.org/10.1109/acc.2002.1023208.

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Mishra, Amardeep, and Nandan Sinha. "Design of Adaptive Sliding Mode Control for Uncertain Thrust Vectored Airship." In 2018 AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1129.

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Yang Junyou, He Guofeng, and Cui Jiefan. "Sliding Mode Variable-structure Direct Thrust Control of PMLSM Using SVM." In Proceedings of the Eighth International Conference on Electrical Machines and Systems. IEEE, 2005. http://dx.doi.org/10.1109/icems.2005.202834.

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4

Mishra, Amardeep, and Nandan Sinha. "Correction: Design of Adaptive Sliding Mode Control for Uncertain Thrust Vectored Airship." In 2018 AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1129.c1.

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Yang, Junyou, Guofeng He, and Jiefan Cui. "Analysis of PMLSM Direct Thrust Control System Based on Sliding Mode Variable Structure." In 2006 5th International Power Electronics and Motion Control Conference. IEEE, 2006. http://dx.doi.org/10.1109/ipemc.2006.297109.

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6

Kamisli, Hamza, Bulent Ozkan, and Metin U. Salamci. "Sliding mode control of an electromechanically-actuated launcher by diminishing the thrust effect." In 2017 International Conference on Mechanical, System and Control Engineering (ICMSC). IEEE, 2017. http://dx.doi.org/10.1109/icmsc.2017.7959462.

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Huang, Yi-Sheng, and Cheng-Chung Sung. "Implementation of a fast terminal sliding mode controller for direct thrust control systems." In 2009 IEEE International Conference on Industrial Technology - (ICIT). IEEE, 2009. http://dx.doi.org/10.1109/icit.2009.4939501.

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Yang, Junyou, Guofeng He, and Jiefan Cui. "Analysis of PMLSM Direct Thrust Control System Based on Sliding Mode Variable Structure." In 2006 CES/IEEE 5th International Power Electronics and Motion Control Conference. IEEE, 2006. http://dx.doi.org/10.1109/ipemc.2006.4778065.

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Rajesh, R. J., Yuri Shtessel, Shamila Nateghi, and Siddharth Sankar Das. "Sensor Performance Improvement via Measured Input Reconstruction Using Sliding Mode Observers." In 2020 IEEE Conference on Control Technology and Applications (CCTA). IEEE, 2020. http://dx.doi.org/10.1109/ccta41146.2020.9206326.

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Chu, Zhenzhong, Daqi Zhu, and Chaomin Luo. "Adaptive neural sliding mode trajectory tracking control for autonomous underwater vehicle without thrust model." In 2017 13th IEEE Conference on Automation Science and Engineering (CASE 2017). IEEE, 2017. http://dx.doi.org/10.1109/coase.2017.8256339.

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