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Journal articles on the topic 'Control system guidance'

Author: Grafiati

Published: 30 May 2022

Last updated: 31 May 2022

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1

Chen, X. L., X. H. Fan, Y. Wang, H. M. Long, T. Jiang, J. Shi, Q. Y. Song, and X. D. Yang. "Control guidance system for sintering burn through point." Ironmaking & Steelmaking 36, no. 3 (April 2009): 209–11. http://dx.doi.org/10.1179/174328107x155367.

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2

Barua, Arindam, M. P. Premchand, R. Vishnu, Prabhat Kumar Dubey, Anon Jayachitra, Ambili K. Gopinath, S. Anitha, et al. "Integrated Navigation, Guidance and Control System and Validation." Current Science 114, no. 01 (January 10, 2018): 109. http://dx.doi.org/10.18520/cs/v114/i01/109-122.

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3

Yakimenko, O., V. Dobrokhodov, J. Johnson, I. Kaminer, S. Delliker, and R. Benney. "GUIDANCE AND CONTROL OF AFFORDABLE GUIDED AIRDROP SYSTEM." IFAC Proceedings Volumes 35, no. 1 (2002): 13–18. http://dx.doi.org/10.3182/20020721-6-es-1901.01228.

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4

Natale, Ciro. "Kinematic Control of Robots with Noisy Guidance System." IFAC Proceedings Volumes 44, no. 1 (January 2011): 6937–44. http://dx.doi.org/10.3182/20110828-6-it-1002.02932.

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5

Moreiras, Daniel Viúdez, and Juan M. Martín Sánchez. "Guidance system for control periods under modelling threshold." International Journal of Automation and Control 10, no. 3 (2016): 215. http://dx.doi.org/10.1504/ijaac.2016.077587.

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6

Chao, Tao, Denghui Zhang, Songyan Wang, and Ping Ma. "Integrated guidance and control design considering system uncertainty." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 233, no. 6 (May 24, 2018): 2278–90. http://dx.doi.org/10.1177/0954410018776512.

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The hypersonic vehicle has the characteristics of strong coupling, high uncertainty and complex nonlinearity, leading to an unsatisfactory control performance with the traditional design method. In this paper, an integrated guidance and control design approach is proposed to cope with this problem. A time-varying longitudinal integrated guidance and control model is first formulated, and then the overall uncertainty consisting of the un-modeled dynamic, parameter uncertainty and external disturbance is taken into account. A novel finite-time extended state observer is developed to estimate and compensate it in real time. Furthermore, an integrated guidance and control algorithm utilizing back-stepping method and the dynamic inverse is put forward. It has been theoretically proved that the finite-time extended state observer system and the cascade system are globally finite-time stable. Numerical simulation results under different kinds of uncertainty with different amplitude and frequency are presented to illustrate the effectiveness and feasibility of the proposed approach. The proposed integrated guidance and control possesses a better convergence performance and stronger disturbance rejection property in existence of the mismatched uncertainty and parameter uncertainty.

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7

Nagasawa, Takashi, Masayuki Hamano, Shinji Shimano, Chihiro Fukui, and Toshiyuki Fujikawa. "Development of restoration guidance system for control centres." International Journal of Electrical Power & Energy Systems 14, no. 2-3 (April 1992): 181–88. http://dx.doi.org/10.1016/0142-0615(92)90043-9.

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8

Binazadeh, T., and M.-J. Yazdanpanah. "Robust partial control design for non-linear control systems: a guidance application." Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 226, no. 2 (September 16, 2011): 233–42. http://dx.doi.org/10.1177/0959651811413013.

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In this paper, a general approach for robust partial stabilization of uncertain non-linear systems is presented. In this approach, the non-linear dynamic system is divided into two subsystems, called the first and the second subsystems. This division is done based on the required stability properties of the system’s states. The reduced input vector (the vector that includes components of the input vector appearing in the first subsystem) is designed to asymptotically stabilize the first subsystem. The proposed scheme is then applied for designing a guidance law as a potential application. Indeed, the paper presents a new approach to the missile guidance problem and shows that asymptotic stability behaviour is not realistic for all states of the guidance system. The effectiveness of the proposed guidance law in interception of manoeuvring targets is demonstrated analytically and through computer simulations.

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9

Wang, Yexing, Humin Lei, Jikun Ye, and Xiangwei Bu. "Backstepping Sliding Mode Control for Radar Seeker Servo System Considering Guidance and Control System." Sensors 18, no. 9 (September 3, 2018): 2927. http://dx.doi.org/10.3390/s18092927.

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This paper investigates the design of a missile seeker servo system combined with a guidance and control system. Firstly, a complete model containing a missile seeker servo system, missile guidance system, and missile control system (SGCS) was creatively proposed. Secondly, a designed high-order tracking differentiator (HTD) was used to estimate states of systems in real time, which guarantees the feasibility of the designed algorithm. To guarantee tracking precision and robustness, backstepping sliding-mode control was adopted. Aiming at the main problem of projectile motion disturbance, an adaptive radial basis function neural network (RBFNN) was proposed to compensate for disturbance. Adaptive RBFNN especially achieves online adjustment of residual error, which promotes estimation precision and eliminates the “chattering phenomenon”. The boundedness of all signals, including estimation error of high-order tracking differentiator, was especially proved via the Lyapunov stability theory, which is more rigorous. Finally, in considered scenarios, line of sight angle (LOSA)-tracking simulations were carried out to verify the tracking performance, and a Monte Carlo miss-distance simulation is presented to validate the effectiveness of the proposed method.

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10

Sun, Rong Chun, Yan Piao, Yu Wang, and Han Wang. "Parking Guidance Control System Based on Internet of Things." Applied Mechanics and Materials 273 (January 2013): 641–45. http://dx.doi.org/10.4028/www.scientific.net/amm.273.641.

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To help drivers to quickly find a spare parking, a parking guidance control system was proposed. The principle of ultrasonic ranging was used to detect the state of a parking space, and through the internet of things the parking detector transmits the real-time information to the control center. The control center mainly is an industrial computer and is responsible for dealing with the real-time information and sending the control command by internet of things. The guidance signs at each crossroad receive the wireless commands and execute them, by which the guidance function is performed. The internet of things was realized by ZigBee star network, in which the control center is a coordinator and other parts are routers or terminal equipments. The simulation experiment results show that the parking guidance system works well, and has the value of application and promotion to some extent.

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11

Gaberdiel, Philip, and Kevin Morley. "Process Control System Security Guidance for the Water Sector." Proceedings of the Water Environment Federation 2014, no. 1 (October 1, 2014): 1–5. http://dx.doi.org/10.2175/193864714816100858.

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12

高, 俊光. "Design of Guidance and Control System for Military Training." Modeling and Simulation 03, no. 04 (2014): 101–9. http://dx.doi.org/10.12677/mos.2014.34014.

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13

Canali, Luis R., Carlos L. Candiani, Eduardo A. Destéfanis, and Mario R. Modesti. "A Simple Control Strategy for an AGV Guidance System." IFAC Proceedings Volumes 28, no. 19 (September 1995): 183–86. http://dx.doi.org/10.1016/s1474-6670(17)45078-6.

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14

Donecker, S. M., T. A. Lasky, and B. Ravani. "A mechatronic sensing system for vehicle guidance and control." IEEE/ASME Transactions on Mechatronics 8, no. 4 (December 2003): 500–510. http://dx.doi.org/10.1109/tmech.2003.820021.

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15

Yamasaki, Takeshi, Hiroyuki Takano, Yoichi Sato, and Yoriaki Baba. "GUIDANCE AND CONTROL SYSTEM FOR POINTING-DEVICE-CONTROLLED AIRCRAFT." IFAC Proceedings Volumes 40, no. 7 (2007): 85–90. http://dx.doi.org/10.3182/20070625-5-fr-2916.00016.

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16

Turetsky, Vladimir, and Tal Shima. "Pursuit-Evasion Guidance in a Switched System." SIAM Journal on Control and Optimization 56, no. 4 (January 2018): 2613–33. http://dx.doi.org/10.1137/17m1142764.

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17

Yun, Changho, Hak-Jin Kim, Chan-Woo Jeon, and Jung-Hun Kim. "Stereovision-Based Guidance Line Detection Method for Auto-guidance system on Furrow Irrigated Fields." IFAC-PapersOnLine 51, no. 17 (2018): 157–61. http://dx.doi.org/10.1016/j.ifacol.2018.08.080.

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18

Zhu, Chenqi, and Zhengyu Guo. "Design of Head-Pursuit Guidance Law Based on Backstepping Sliding Mode Control." International Journal of Aerospace Engineering 2019 (December 3, 2019): 1–18. http://dx.doi.org/10.1155/2019/8214042.

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In order to meet the needs of high-precision guidance for intercepting hypersonic targets, a novel head-pursuit guidance law considering the dynamic characteristics of a missile control system and the target mobility is presented via combining a fast power reaching law with backstepping sliding mode control in this paper. Initially, a three-dimensional head-pursuit system model of the missile and target is established. Subsequently, the system model is decomposed into a pitch plane system and lateral plane system, the control system dynamics are equivalent to second-order systems, and finite-time disturbance observers are introduced to estimate the target accelerations. On the basis of the previous work, the head-pursuit guidance laws of the vertical system and the lateral system which can stabilize the closed-loop system are designed separately and strict proofs of the methods are given. Finally, simulations are carried out to verify the effectiveness of this head-pursuit guidance law.

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19

Gurfil, P. "Non-linear missile guidance synthesis using control Lyapunov functions." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 219, no. 2 (February 1, 2005): 77–87. http://dx.doi.org/10.1243/095441005x9085.

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This paper derives a new non-linear guidance law aimed at interception of highly manoeuvring targets. The guidance law is developed based on the theory of control Lyapunov functions (CLFs), a methodology for universal stabilization of non-linear systems which is also inverse optimal with respect to some performance measure. The three-dimensional guidance dynamics are formulated in a fixed-line-of-sight coordinate system, yielding matching between the target and missile accelerations. Closed-form expressions for the CLF guidance commands are given. Simulation shows that the new guidance scheme significantly outperforms augmented proportional navigation in short-range engagements.

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20

Cao, Jian, Cong Yan, and Jian He Li. "Integrated Design about Guidance and Control in Inversible System of Neural Network." Applied Mechanics and Materials 415 (September 2013): 294–97. http://dx.doi.org/10.4028/www.scientific.net/amm.415.294.

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Integrated design about guidance and control in inversible system of neural network is proposed. Firstly, an integrated guidance and control model with uncertainties can be described. Secondly, a nonlinear observer is designed for the integrated guidance and control model. Subsequently, selection of training sample is focused on. Finally, the simulation results show that the nonlinear adaptive guidance law using the proposed integrated design model can perform better than the one designed separately.

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21

Wang, Yi, Ge Yu, Guan-Yang Liu, Chao Huang, and Yu-Hang Wang. "Vibrotactile-Based Operational Guidance System for Space Science Experiments." Actuators 10, no. 9 (September 9, 2021): 229. http://dx.doi.org/10.3390/act10090229.

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On-orbit astronauts and scientists on the ground need to cooperate closely, to complete space science experiments efficiently. However, for the increasingly diverse space science experiments, scientists are unable to train astronauts on the ground about the details of each experiment. The traditional interaction of visual and auditory channels is not enough for scientists to directly guide astronauts to experimentalize. An intuitive and transparent interaction interface between scientists and astronauts has to be built to meet the requirements of space science experiments. Therefore, this paper proposed a vibrotactile guidance system for cooperation between scientists and astronauts. We utilized Kinect V2 sensors to track the movements of the participants of space science experiments, process data in the virtual experimental environment developed by Unity 3D, and provide astronauts with different guidance instructions using the wearable vibrotactile device. Compared with other schemes using only visual and auditory channels, our approach provides more direct and more efficient guidance information that astronauts perceive is what they need to perform different tasks. Three virtual space science experiment tasks verified the feasibility of the vibrotactile operational guidance system. Participants were able to complete the experimental task with a short period of training, and the experimental results show that the method has an application prospect.

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22

Marchetti, Francesco, and Edmondo Minisci. "Genetic Programming Guidance Control System for a Reentry Vehicle under Uncertainties." Mathematics 9, no. 16 (August 6, 2021): 1868. http://dx.doi.org/10.3390/math9161868.

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As technology improves, the complexity of controlled systems increases as well. Alongside it, these systems need to face new challenges, which are made available by this technology advancement. To overcome these challenges, the incorporation of AI into control systems is changing its status, from being just an experiment made in academia, towards a necessity. Several methods to perform this integration of AI into control systems have been considered in the past. In this work, an approach involving GP to produce, offline, a control law for a reentry vehicle in the presence of uncertainties on the environment and plant models is studied, implemented and tested. The results show the robustness of the proposed approach, which is capable of producing a control law of a complex nonlinear system in the presence of big uncertainties. This research aims to describe and analyze the effectiveness of a control approach to generate a nonlinear control law for a highly nonlinear system in an automated way. Such an approach would benefit the control practitioners by providing an alternative to classical control approaches, without having to rely on linearization techniques.

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23

Liu, Peng, Cheng Yuan Peng, Ge Li, Feng Xue, and Jia Qi Liu. "Research on Extra-Atmospheric Aircraft Modeling and Control Based on Maneuvering Target." Applied Mechanics and Materials 799-800 (October 2015): 1142–48. http://dx.doi.org/10.4028/www.scientific.net/amm.799-800.1142.

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The extra-atmospheric aircraft model is established, and then the control system is designed. The control system consist of attitude control system and orbit control system, the attitude control system used PID controller and the orbit control system used augmented proportional navigation method. The traditional Proportional Navigation (PN) guidance law has higher accuracy. But for highly maneuvering targets, the accuracy of traditional PN guidance law is still not enough. An Augmented Proportional Navigation (APN) guidance law is designed, an acceleration compensation of the target is introduced on the basis of PN guidance law to overcome the effect of the acceleration on the guidance accuracy. And the engine control method is designed based on the fixed engine thrust. Simulation results indicated that, for homing against maneuverable targets, the APN guidance law is better than the PN guidance law in the following aspects: guidance accuracy is higher, miss distance is lower, interception time is shorter. And the new guidance law provides significant performance improvements over the commonly used classical proportional navigation law.

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24

O'Hara, John, William Brown, William Stubler, James Higgins, Jerry Wachtel, and J. J. Persensky. "Human Factors Guidance for Control Room Evaluation." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 44, no. 22 (July 2000): 519–22. http://dx.doi.org/10.1177/154193120004402205.

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The Human-System Interface Design Review Guideline (NUREG-0700, Revision 1) was developed by the U.S. Nuclear Regulatory Commission (NRC) to provide human factors guidance as a basis for the review of advanced human-system interface technologies. The guidance consists of three components: design review procedures, human factors engineering guidelines, and a software application to provide design review support called the “Design Review Guideline.” Since it was published in June 1996, Rev. 1 to NUREG-0700 has been used successfully by NRC staff, contractors and nuclear industry organizations, as well as by interested organizations outside the nuclear industry. The NRC has committed to the periodic update and improvement of the guidance to ensure that it remains a state-of-the-art design evaluation tool in the face of emerging and rapidly changing technology. This paper addresses the current research to update of NUREG-0700 based on the substantial work that has taken place since the publication of Revision 1.

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25

Hu, Shu Guang, Chang Cheng Li, Shao Yang Yan, and Xin Xin. "Study on Control Strategy of Intelligent Guidance System for Foggy Area Traffic Safety." Applied Mechanics and Materials 209-211 (October 2012): 654–62. http://dx.doi.org/10.4028/www.scientific.net/amm.209-211.654.

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In recent years, an innovative Intelligent Guidance System for traffic safety under limited visibility conditions appeared and evolved. According to prevailing visibility and traffic conditions, such systems can provide roadway outline reinforcement, vehicle active guidance, rear-end collision warning functions by changing brightness, color, flashing frequency, etc. of the illuminant guidance facilities. Rear-end collision warning function is the marked feature different from traditional guidance facilities. This paper elaborates main principle, system configuration, word mode, control strategy of such system. Especially, emphasis is put on the analysis of key control parameters such as threshold of red lamp duration, quantity of trigged red lamps, which impact practical effects of such system greatly. Regarding the particular rear-end collision warning function, the author use time series chart of trigged red lamps status and list table of key parameters change to induce and optimize key control parameters configuration. The relationship of safe spacing between vehicles, advised speed limit, threshold of red lamp duration and quantity of trigged red lamps is established. And this can be referred to improve the practical effectiveness when such systems are constructed and used.

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26

Feldmann, Klaus, Matthias Wenk, and Josef Zeller. "Fast sensor guidance of industrial robots – experimental results." Robotica 17, no. 1 (January 1999): 17–21. http://dx.doi.org/10.1017/s0263574799001010.

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For securing and increasing the quality of various material processing technologies a flexible sensor data integration is indispensable. Hence, a powerful and configurable sensor-robot-system was designed and implemented, integrating sensor data into industrial robot controls within the interpolation or the position control clock rate. Different controllers were designed and the system responses of the control loops were simulated and optimized by an efficient control design tool. Experimental results on the achievable path accuracy are presented. Finally, some application for the developed sensor control loops are introduced.

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27

Duhri, Rahmat Alfi, Rianto Adhy Sasongko, and Yayom Dwi Laksmana. "Design and Simulation of Air to Air Missile Homing System." INSIST 2, no. 2 (January 25, 2019): 75. http://dx.doi.org/10.23960/ins.v2i2.84.

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This paper will talk about AIM 120 AMRAAM missile guidance for pursuing a moving target. The missile guidance system itself consists of missile dynamics, control system, seeker, and guidance methods. For general purpose, the missile dynamics approach will use non-linear equation of motions. The control surface that will be discussed follow the rule BTT (Bank-to-Turn) and control system that will be used is PID control system that widely used for control design. Lastly, the guidance method that will be studied here is proportional navigation and constant bearing course approach. The simulation will be conducted using MATLAB Simulink. The Simulink model consist of target dynamics, and guidance system. From the result of simulation, it will be shown that the missile can pursue its target quite well. Hence, the simulation system can be used well for preliminary design purpose.Keywords—Homing System, Control System, Proportional Navigation, Missile Dynamics, Seeker, Bank-to-Turn, Constant Bearing Course.

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28

Açıkmeşe, Behçet, Steven W. Sell, A. Miguel San Martin, and Jeffrey J. Biesiadecki. "Mars Science Laboratory Flyaway Guidance, Navigation, and Control System Design." Journal of Spacecraft and Rockets 51, no. 4 (July 2014): 1227–36. http://dx.doi.org/10.2514/1.a32709.

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29

Kazurova, A. E., and E. M. Potapenko. "Robust control system of armored vehicle armament guidance and stabilization." Electrical Engineering and Power Engineering, no. 1 (July 22, 2011): 18–26. http://dx.doi.org/10.15588/1607-6761-2011-1-3.

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30

Zhang, Man, Wenqiang Ma, Zhaoxiang Liu, and Gang Liu. "Fuzzy-adaptive control method for off-road vehicle guidance system." Mathematical and Computer Modelling 58, no. 3-4 (August 2013): 551–55. http://dx.doi.org/10.1016/j.mcm.2011.10.066.

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31

Shan, Guangbao, Guodong Wang, Qijun Lu, and Yintang Yang. "A 3D heterogeneously integrated guidance, navigation, and control micro-system." Japanese Journal of Applied Physics 58, SH (June 11, 2019): SHCB01. http://dx.doi.org/10.7567/1347-4065/ab17c3.

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32

Roberts, G. W., A. H. Dodson, and V. Ashkenazi. "Global Positioning System aided autonomous construction plant control and guidance." Automation in Construction 8, no. 5 (June 1999): 589–95. http://dx.doi.org/10.1016/s0926-5805(99)00008-4.

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33

Ninomiya, Tetsujiro, Hirokazu Suzuki, and Jun'ichiro Kawaguchi. "Evaluation of Guidance and Control System of D–SEND#2." IFAC-PapersOnLine 49, no. 17 (2016): 106–11. http://dx.doi.org/10.1016/j.ifacol.2016.09.019.

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34

Park, Chul-Woo, Il-Hyung Park, and Sanghyun Joung. "Control Method of Surgical Instrument Guidance System Using Line Laser." Journal of Korean Institute of Information Technology 16, no. 5 (May 31, 2018): 29–37. http://dx.doi.org/10.14801/jkiit.2018.16.5.29.

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35

Harris, C. J., X. Hong, and P. A. Wilson. "An intelligent guidance and control system for ship obstacle avoidance." Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering 213, no. 4 (June 1999): 311–20. http://dx.doi.org/10.1243/0959651991540179.

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36

Kaminer, Isaac, and Patrick O'Shaughnessy. "Integration of four-dimensional guidance with total energy control system." Journal of Guidance, Control, and Dynamics 14, no. 3 (May 1991): 564–73. http://dx.doi.org/10.2514/3.20676.

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37

Wang, Yi, Xiaohui Fan, and Xuling Chen. "Expert System for Control Guidance of Grate-Kiln Pellet Production." ISIJ International 53, no. 3 (2013): 399–402. http://dx.doi.org/10.2355/isijinternational.53.399.

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38

Peng, Zheng Hong, and Jin Jun Xu. "Research on Traffic Guidance and Control System Coordinated Agent Model." Applied Mechanics and Materials 97-98 (September 2011): 872–76. http://dx.doi.org/10.4028/www.scientific.net/amm.97-98.872.

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Traffic problem is one of serious problem in our society. Put forward the concept of intelligent transportation systems, is seeking to address traffic problems, and gradually become a research hotspot in traffic areas. As two subsystems, traffic control and traffic guidance systems tend to work independently, this paper aims to establish a coordination with the integration of the two systems, while use the agent technologies which emergy in artificial intelligence to establish an integrated model.

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39

Ueno, Mami. "A GPS-based system for precise shipping guidance and control." Journal of Marine Science and Technology 5, no. 1 (October 16, 2000): 9–15. http://dx.doi.org/10.1007/s007730070016.

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40

Dadkhah, Navid, and Bérénice Mettler. "Control system design and evaluation for robust autonomous rotorcraft guidance." Control Engineering Practice 21, no. 11 (November 2013): 1488–506. http://dx.doi.org/10.1016/j.conengprac.2013.04.011.

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41

Li, Chaoyong, Wuxing Jing, Hui Wang, and Zhiguo Qi. "Development of flight control system for 2D differential geometric guidance and control problem." Aircraft Engineering and Aerospace Technology 79, no. 1 (January 30, 2007): 60–68. http://dx.doi.org/10.1108/00022660710720502.

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42

Guo, Jianguo, Yu Xiong, and Jun Zhou. "A new sliding mode control design for integrated missile guidance and control system." Aerospace Science and Technology 78 (July 2018): 54–61. http://dx.doi.org/10.1016/j.ast.2018.03.042.

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43

Shima, T., and O. M. Golan. "End-game guidance laws for dual-control missiles." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 219, no. 2 (February 1, 2005): 157–70. http://dx.doi.org/10.1243/095441005x7249.

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New guidance laws derived for a dual-control missile are studied. Their performance is compared with that of a conventional guidance system with flight control that distributes the commands among the two control channels. A Monte Carlo simulation study is performed where the target executes random evasive manoeuvres. The interceptor, represented by linear high-order manoeuvring dynamics with bounded forward and aft controls, acquires noisy measurements and uses a state estimator. Using the single-shot kill probability as a performance criterion, the superiority of the new guidance and control architecture is shown. It is also shown that the best performance is obtained by the bounded controls differential game guidance law. Sensitivity to the selection of the interceptor first-order time constant, a design parameter in the guidance law derivation, is also investigated.

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44

Głębocki, R. "Guidance impulse algorithms for air bomb control." Bulletin of the Polish Academy of Sciences: Technical Sciences 60, no. 4 (December 1, 2012): 825–33. http://dx.doi.org/10.2478/v10175-012-0096-4.

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Abstract In this paper, some results of research concerning the development of guidance of bombs were presented. The paper presents conceptions of an impulse (gasodynamic) control system, the measurement unit based on IMU/GPS signals and control algorithms based on predicted trajectories. The presented results of simulation research are based on the numerical model of the bomb and real signals from measurement devices.

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45

Sun, Rong Chun, and Yan Piao. "Parking Guidance System Based on RFID." Advanced Materials Research 860-863 (December 2013): 2787–90. http://dx.doi.org/10.4028/www.scientific.net/amr.860-863.2787.

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With the rapid increase of vehicles, the problem of parking has become very serious. So to guidance drivers to park is significant. A parking guidance system was proposed. Firstly, parking place is divided into different regions. Then the state of the parking space in a parking region is detected by ultrasound sensor, and the state of the parking region in a parking is detected by RFID reader. Through the internet of things, the state information is transmitted to the control center in real time that mainly is an industrial computer and is responsible for dealing with the state information and sending guidance commands to displaying signs, which are at crossroad and guidance passing cars. The experiment results show that the parking guidance system works well, and has the value of application and promotion to some extent.

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46

Zhang, Honghua, Ji Li, Zeguo Wang, and Yifeng Guan. "Guidance Navigation and Control for Chang’E-5 Powered Descent." Space: Science & Technology 2021 (July 13, 2021): 1–15. http://dx.doi.org/10.34133/2021/9823609.

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To achieve the goal of collecting lunar samples and return to the Earth for the Chang’E-5 spacecraft, the lander and ascender module (LAM) of the Chang’E-5 spacecraft successfully landed on the lunar surface on 1 Dec., 2020. The guidance, navigation, and control (GNC) system is one of the critical systems to perform this task. The GNC system of previous missions, Chang’E-3 and Chang’E-4, provides the baseline design for the Chang’E-5 LAM, and the new characteristics of the LAM, like larger mass and liquid sloshing, also bring new challenges for the GNC design. The GNC design for the descent and landing is presented in this paper. The guidance methods implemented in the powered descent are presented in detail for each phase. Propellant consumption and hazard avoidance should be particularly considered in the design. A reconfigurable attitude control is adopted which consists of the quaternion partition control, phase and gain stabilization filter, and dual observer. This controller could provide fast attitude maneuver and better system robustness. For the navigation, an intelligent heterogeneous sensor data fusion method is presented, and it is applied for the inertial measurement unit and velocimeter data. Finally, the flight results of the LAM are shown. Navigation sensors were able to provide valid measurement data during descent, and the thrusters and the main engine operated well as expected. Therefore, a successful soft lunar landing was achieved by the LAM.

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47

Huang, Hanqiao, Xin Zhao, and Xiaoyan Zhang. "Intelligent Guidance and Control Methods for Missile Swarm." Computational Intelligence and Neuroscience 2022 (January 25, 2022): 1–9. http://dx.doi.org/10.1155/2022/8235148.

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High-speed unmanned aerial vehicles (UAVs) are more and more widely used in both military and civil fields at present, especially the missile swarm attack, and will play an irreplaceable key role in the future war as a special combat mode. This study summarizes the guidance and control methods of missile swarm attack operation. First, the traditional design ideas of the guidance and control system are introduced; then, the typical swarm attack guidance and control methods are analyzed by taking their respective characteristics into considering, and the limitations of the traditional design methods are given. On this basis, the study focuses on the advantages of intelligent integrated guidance and control design over traditional design ideas, summarizes the commonly used integrated guidance and control design methods and their applications, and explores the cooperative attack strategy of missile swarm suitable for the integrated guidance and control system. Finally, the challenges of missile swarm guidance and control are described, and the problems worthy of further research in the future are prospected. Summarizing the guidance and control methods of missile will contribute to the innovative research in this field, so as to promote the rapid development of unmanned swarm attack technology.

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Yue, Wenchao, Ruijie Tang, Joei Simin Wong, and Hongliang Ren. "Deployable Tubular Mechanisms Integrated with Magnetic Anchoring and Guidance System." Actuators 11, no. 5 (April 28, 2022): 124. http://dx.doi.org/10.3390/act11050124.

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Deployable mechanism has received more attention in the medical field due to its simple structure, dexterity, and flexibility. Meanwhile, the advantages of the Magnetic Anchoring and Guidance System (MAGS) are further highlighted by the fact that the operators can remotely control the corresponding active and passive magnetic parts in vivo. Additionally, MAGS allows the untethered manipulation of intracorporeal devices. However, the conventional instruments in MAGS are normally rigid, compact, and less flexible. Therefore, to solve this problem, four novel deployable tubular mechanisms, Design 1 (Omega-shape mechanism), Design 2 (Fulcrum-shape mechanism), Design 3 (Archway-shape mechanism), and Design 4 (Scissor-shape mechanism) in this paper, are proposed integrated with MAGS to realize the laser steering capability. Firstly, this paper introduces the motion mechanism of the four designs and analyzes the motion characterization of each structure through simulation studies. Further, the prototypes of four designs are fabricated using tubular structures with embedded magnets. The actuation success rate, the workspace characterization, the force generation and the load capability of four mechanisms are tested and analyzed based on experiments. Then, the demonstration of direct laser steering via macro setup shows that the four mechanisms can realize the laser steering capability within the error of 0.6 cm. Finally, the feasibility of indirect laser steering via a macro-mini setup is proven. Therefore, such exploration demonstrates that the application of the deployable tubular mechanisms integrated with MAGS towards in vivo treatment is promising.

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Fugui, Li, Jia Shengwei, Tong Zeyou, Zhao Changjian, Li Yahui, Gao Feng, and Gong Min. "Guidance and Control Method for Vehicle with Strap-down Seeker." MATEC Web of Conferences 291 (2019): 01003. http://dx.doi.org/10.1051/matecconf/201929101003.

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Guidance and control method was presented in this paper for flight vehicle with a strap-down seeker. Firstly, an extended Kalman filter was constructed in LOS (line of sight) coordinate system to estimate the guidance signal based on the information measured by strap-down seeker and inertial measurement unit. Secondly, an optimal guidance law which could reduce the target maneuvering and guidance system dynamics was proposed. Thirdly, three-loop acceleration autopilot with pseudo-angle of attack feedback was presented to control the flight vehicle. Finally, the proposed methods were simulated under typical condition. The simulation results demonstrated that the proposed methods were valid, and good performance could be achieved by the guidance and control method with the guidance signal estimated by the extended Kalman filter.

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Wang, Chun Xia, Xian Sheng Qin, Zhong Xia Qi, and Wen Hui Liu. "The System Control Model Based on Biological DNA." Advanced Materials Research 403-408 (November 2011): 3631–35. http://dx.doi.org/10.4028/www.scientific.net/amr.403-408.3631.

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In order to increase autonomy and adaptive system, this article builds a control model based on biological mechanism of DNA. In the cell gene controls the characteristics of the organism by guidance to synthesis of proteins. On the basis of the research in the biological regulation of DNA expression and mechanism, building cell control model based on Petri nets, sketch-like cell control system design of basic ideas and principles, and the article provides a modeling method to improve system performance.

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