Relevant bibliographies by topics / Aircraft - Automatic Control

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Aircraft - Automatic Control'

Author: Grafiati
Published: 4 June 2021
Last updated: 7 September 2023

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Journal articles on the topic "Aircraft - Automatic Control"

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Suhih, Nikolai, and Valentin Rukavishnikov. "Research of the Processes of Aircraft Director Control at Board Calculator Failure." Automation on transport 8, no. 2 (2022): 121–32. http://dx.doi.org/10.20295/2412-9186-2022-8-2-121-132.

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It’s accepted to divide aircraft automatic control into semi-automatic (director) and automatic. Semi-automatic (director) systems provide for the collection and analysis of information, delivered from navigation equipment. On aircraft position in space and give a command to a pilot. Aircraft management with the help of such piloting-navigational systems is called semi-automatic because information collection and processing on aircraft condition is automated but the control’s left to be manual. Automatic control systems provide not just for information collection and processing on aircraft state but also for management laws as well as for control process itself. A man implements functions on automatic system work control, on identifying, making decisions on inclusion of this or that program, function of "hot" reserve. Present article shows experiment organization and obtained results on research of the processes of airplane director management while failures of board calculator of trajectory control system with real pilot inclusion into circuit. The research is held on the stage of aircraft approach and landing. The experiment was held on special bench of half-real modeling.
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Šlihta, Mareks, Vladimirs Šestakovs, and Ramachandran Karunanidhi. "Aircraft Automatic Control System Failure and Flight Safety." Transport and Aerospace Engineering 3, no. 1 (2016): 15–23. http://dx.doi.org/10.1515/tae-2016-0002.

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Abstract This article presents a mathematical model estimating the probability of successful completion of the aircraft’s flight in case of aviation equipment failure in flight. This paper shows the relationship between the aircraft’s automatic control system and flight safety. The calculations of probability are made for the successful completion of the flight on Boeing 737 aircraft when the automatic control system has failed.
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Yamasaki, Takeshi, Keisuke Enomoto, Daiki Tanaka, Daiki Tanaka, and Yoriaki Baba. "Automatic Control for Chase Aircraft." International Journal of Aeronautical and Space Sciences 7, no. 2 (2006): 145–54. http://dx.doi.org/10.5139/ijass.2006.7.2.145.

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Zajdel, Albert, Cezary Szczepański, Mariusz Krawczyk, Jerzy Graffstein, and Piotr Masłowski. "Selected Aspects of the Low Level Automatic Taxi Control System Concept." Transactions on Aerospace Research 2017, no. 2 (2017): 69–79. http://dx.doi.org/10.2478/tar-2017-0016.

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Abstract Taxiing of manned and remotely piloted aircraft is still performed by pilots without using a system of automatic control of direction and speed. Several reasons have emerged in recent years that make the automation of taxiing an important design challenge. The reasons are: decreased airport capacity due to the growing number of aircraft, poor ground operation conditions during poor visibility conditions, an increase in workload of pilots and air traffic controllers and the integration of simultaneous ground operations of manned and remotely piloted air vehicles. This paper presents selected aspects of the concept of a Low Level Automatic Taxi Control System. In particular, it emphasizes the means of controlling an aircraft during taxiing, accuracy requirements of the system and proposes control techniques. The resulting controller of the system is adaptable for different aircrafts. The actuators and their mechanical connections to available controls are the aircraft specific part and are designed for the particular type – in this case – a general aviation light airplane.
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Krawczyk, Mariusz, Cezary Szczepański, and Albert Zajdel. "Automatic Taxiing Direction Control System for Carrier-Based Aircraft." Transactions on Maritime Science 8, no. 2 (2019): 171–79. http://dx.doi.org/10.7225/toms.v08.n02.002.

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This paper solves the problem of automatic taxiing direction control of carrier-based aircraft. On modern aircraft carriers, taxiing aircraft either propel themselves using their own engines or are towed by specialised tugs, which requires dedicated personnel and assets. The automatization of this process would simultaneously increase aircraft flow and decrease the number of personnel and assets required. The key challenge in the automatization of this type of process is the development of an automatic control system capable of performing the requisite tasks, which our researchers managed to do. First, the specific conditions of taxiing on-board carriers were analysed and modelled. The model of a fixed-wing aircraft best suited to this purpose was identified and the proper method of automatic control – ADRC – chosen. The algorithm used in the methodto facilitate effective direction control of a taxiing aircraft was formulated and extensively tested. The results of automatic taxiing simulation for F/A-18 aircraft have been presented. The conclusion is that the ADRC type control algorithm can ensure effective automatic control of taxiing aircraft.
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Zhen, Ziyang, Ju Jiang, Xinhua Wang, and Kangwei Li. "Modeling, control design, and influence analysis of catapult-assisted take-off process for carrier-based aircrafts." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 13 (2017): 2527–40. http://dx.doi.org/10.1177/0954410017715278.

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This paper addresses the problems of modeling, control design, and influence analysis of the steam catapult-assisted take-off process of the carrier-based aircrafts. The mathematical models of the carrier-based aircraft, steam catapult, landing gears, and the environmental factors including deck motion and bow airflow have been established to express the aircraft dynamics in the take-off process. An engineering method based automatic flight control system has been designed, which is divided into the longitudinal channel and lateral channel. The influences of the preset control surface, ship deck motion, ship bow airflow, and automatic flight control system system are tested by a series of simulations. The simulation results show that the elevator angle preset is necessary in the stage of accelerated running on the ship deck and the deck motion is the most important factor for safe take-off, while the ship bow airflow is beneficial for climbing up of the aircraft. The automatic flight control system gives the guarantee of safety and performance in the take-off process of the carrier-based aircraft.
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Rogalski, Tomasz. "Unmanned aircraft automatic flight control algorithm in loop manoeuvre." Aircraft Engineering and Aerospace Technology 90, no. 6 (2018): 877–84. http://dx.doi.org/10.1108/aeat-02-2018-0088.

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Purpose This paper aims to present the idea of an automatic control system dedicated to small manned and unmanned aircraft performing manoeuvres other than those necessary to perform a so-called standard flight. The character of these manoeuvres and the range of aircraft flight parameter changes restrict application of standard control algorithms. In many cases, they also limit the possibility to acquire complete information about aircraft flight parameters. This paper analyses an alternative solution that can be applied in such cases. The loop manoeuvre, an element of aerobatic flight, was selected as a working example. Design/methodology/approach This paper used theoretical discussion and breakdowns to create basics for designing structures of control algorithms. A simplified analytical approach was then applied to tune regulators. Research results were verified in a series of computer-based software-in-the-loop rig test computer simulations. Findings The structure of the control system enabling aerobatic flight was found and the method for tuning regulators was also created. Practical implications The findings could be a foundation for autopilots working in non-conventional flight scenarios and automatic aircraft recovery systems. Originality/value This paper presents the author’s original approach to aircraft automated control where high precision control is not the priority and flight parameters cannot be precisely measured or determined.
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Bobin, A. V., V. A. Azarov, S. A. Bulgakov, and D. A. Savin. "Technique for recognition of aircrafts and radar traps in the control circuit of airspace control system based on neural network technology." Izvestiya MGTU MAMI 7, no. 1-4 (2013): 124–30. http://dx.doi.org/10.17816/2074-0530-67843.

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The paper proposes a method for building of automatic recognizers of aircrafts on a set of radar measurements based on the cascade of multilayer feedforward neural networks. The practical application of this technique in recognizing of three types of aircraft is presented as well.
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TUDOSIE, Alexandru Nicolae, and Mádálina Luciana PĂUNESCU. "AUTOMATIC CONTROL SYSTEM FOR AN AIRCRAFT PLAN SUPERSONIC INLET WITH MOBILE PANEL." SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE 19, no. 1 (2017): 243–52. http://dx.doi.org/10.19062/2247-3173.2017.19.1.27.

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Zajdel, Albert, Mariusz Krawczyk, and Cezary Szczepański. "Trim Tab Flight Stabilisation System Performance Assessment under Degraded Actuator Speeds." Aerospace 10, no. 5 (2023): 429. http://dx.doi.org/10.3390/aerospace10050429.

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One of the areas involved in changing current aircraft into more electric ones is decreasing energy consumption by the aircraft’s automatic flight control. Therefore, some aircraft types have tested the possibility of controlling the flight in automatic mode or stabilising the flight with trimmers. Previous research on cost-effective and less electrical-energy-consuming automatic stabilisation systems for an aircraft resulted in constructing a laboratory model of the system. Such a feature is beneficial for initiatives like Future Sky, electric aircraft and aircraft stabilisation system retrofits. The system was developed using model-based design and next tuned and tested in model, pilot and hardware-in-the-loop simulations. The implementation of this system does not modify the pilot’s primary manual controls. Instead, the electrical trim system is used for automatic stabilisation or manual trimming, depending on the chosen operation mode. The paper presents the development process of the laboratory model of the system and its simulation under degraded actuator speeds. The results were the basis for its control performance assessment. First, the control performance measure was defined. Then the simulation scenarios that compare system behaviour in stabilisation mode after aerodynamic disturbance with three different trim tab actuator speeds were described. The performance measure is highly degraded by the slower actuator speeds, although altitude and heading are finally stabilised in all cases. Moreover, the performance of stabilisation in a lateral channel is less affected by the slowest actuator than in a longitudinal channel.
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Dissertations / Theses on the topic "Aircraft - Automatic Control"

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Mukherjee, Jason. "Automatic control of an aircraft employing outboard horizontal stabilizers." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape3/PQDD_0027/NQ49523.pdf.

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Benkhedda, Hassen. "Design of a transport aircraft automatic flight control system with analytical redundancy." Thesis, University of Southampton, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.241599.

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Alkhatib, K. Y. "Analytical redundancy scheme for improving reliability of automatic flight control systems for aircraft." Thesis, Loughborough University, 1985. https://dspace.lboro.ac.uk/2134/31989.

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Any redundancy scheme in aircraft control systems is usually considered separately from the control algorithms involved. All feedback control systems are usually designed under the assumption that their sensors will not fail. When the integrity requirements demand it, then a redundancy scheme must be designed to provide any required measurements with only extremely short interruptions to normal service being caused by failures of individual sensors.
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Tang, Yi Rui. "Development, dynamic modeling, and autonomous flight control of small UAV helicopters." Thesis, University of Macau, 2017. http://umaclib3.umac.mo/record=b3691051.

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Lindblom, Markus. "Semi-Automatic Generation of Control Law Parameters for Generic Fighter Aircraft." Thesis, Linköpings universitet, Reglerteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-167725.

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Control law design can be an iterative and time-consuming process. The design procedure can often include manual tuning, not uncommonly in the form of trial and error. Modern software tools may alleviate this process but are generally not developed for use within any specific industry. There is therefore an apparent need to develop field-specific tools to facilitate control law design.The main contribution of this thesis is the investigation of a systematic and simplified approach to semi-automatic generation of control law parameters for generic fighter aircraft. The investigated method aims to reduce human workload and time spent on complex decision making in the early stages of aircraft development. The method presented is based on gain scheduled LQI-control with piece-wise linear interpolation. A solution to the automated tuning problem of the associated weighting matrices Q and R is investigated. The method is based on an LQ-optimal eigenstructure assignment. However, the derived method suffers from problem regarding practical implementation, such as the seemingly narrow LQ-optimal root-loci of the linearized aircraft model.Furthermore, the inherent problem of hidden coupling is discussed in relation to gain scheduled controllers based on conventional series expansion linearization. An alternative linearization method is used in order to circumvent this problem. Moreover, the possible benefits and disadvantages of control allocation is addressed in the context of actuator redundancy. It is concluded that one may achieve a somewhat simpler handling of constraints at the expense of some model accuracy due to the inevitable exclusion of servo dynamics.
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Zhao, Yue. "Automatic Prevention and Recovery of Aircraft Loss-of-Control by a Hybrid Control Approach." Ohio University / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1458728101.

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Wagner, Elaine Ann. "On-board automatic aid and advisory for pilots of control-impaired aircraft." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/35940.

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Zaludin, Zairil A. "Flight dynamics and automatic flight control system of an hypersonic transport aircraft." Thesis, University of Southampton, 1999. https://eprints.soton.ac.uk/47120/.

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S, Kulik M., Antonov V. K, Glazok O. M, et al. "Unmanned aircraft with a closed wing." Thesis, IEEE, 2015. http://er.nau.edu.ua/handle/NAU/22133.

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A configuration of an unmanned aircraft with closed wing is considered. The method of identification designed for researching the aerodynamic qualities of the model is proposed.<br>http://ieeexplore.ieee.org/xpl/login.jsp?tp=&arnumber=7346558&url=http%3A%2F%2Fieeexplore.ieee.org%2Fxpls%2Ficp.jsp%3Farnumber%3D7346558
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Lim, Bock-Aeng. "Design and rapid prototyping of flight control and navigation system for an unmanned aerial vehicle." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2002. http://sirsi.nps.navy.mil/uhtbin/hyperion-image/02Mar%5FLimBA.pdf.

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Books on the topic "Aircraft - Automatic Control"

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Blakelock, John H. Automatic control of aircraft and missiles. 2nd ed. Wiley, 1991.

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P, Looze D., ed. Automatic control design procedures for restructurable aircraft control. NASA Langley Research Center, 1985.

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Nelson, Robert C. Flight stability and automatic control. 2nd ed. WCB/McGraw Hill, 1998.

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Nelson, Robert C. Flight stability and automatic control. McGraw-Hill, 1989.

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1950-, Stojić R., ed. Modern aircraft flight control. Springer-Verlag, 1988.

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C, Chenoweth C., ed. Aircraft flight control actuation system design. Society of Automotive Engineers, 1993.

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Center, Langley Research, ed. Automatic braking system modification for the Advanced Transport Operating System (ATOPS) Transportation System Research Vehicle (TSRV). National Aeronautics and Space Administration, Langley Research Center, 1986.

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Srinathkumar, S. Eigenstructure control algorithms: Applications to aircraft/ rotorcraft handling qualities design. Institution of Engineering and Technology, 2011.

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Lozano, R. Unmanned aerial vehicles: Embedded control. ISTE, 2010.

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Weihua, Zhang, ed. Wu ren fei xing kong zhi xi tong shi yan jiao cheng. Guo fang gong ye chu ban she, 2011.

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Book chapters on the topic "Aircraft - Automatic Control"

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L’Afflitto, Andrea. "Aircraft Automatic Control." In A Mathematical Perspective on Flight Dynamics and Control. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-47467-0_3.

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Tewari, Ashish. "Automatic Control of Aircraft." In Automatic Control of Atmospheric and Space Flight Vehicles. Birkhäuser Boston, 2011. http://dx.doi.org/10.1007/978-0-8176-4864-0_4.

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Samolej, Sławomir, Marek Orkisz, and Tomasz Rogalski. "The Airspeed Automatic Control Algorithm for Small Aircraft." In Advanced Technologies in Practical Applications for National Security. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-64674-9_10.

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Cai, Jianping, Lujuan Shen, Ye Bao, and Yijun Zhang. "Robust Adaptive Control for a Class of Uncertain Aircraft Systems." In 2011 International Conference in Electrics, Communication and Automatic Control Proceedings. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-8849-2_101.

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Lamp, Maxim, and Robert Luckner. "Automatic Landing of a High-Aspect-Ratio Aircraft without Using the Thrust." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_32.

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Karlsson, Erik, Simon P. Schatz, Thaddäus Baier, et al. "Development of an Automatic Flight Path Controller for a DA42 General Aviation Aircraft." In Advances in Aerospace Guidance, Navigation and Control. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-65283-2_7.

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Gonçalves, Tiago F., José R. Azinheira, and Patrick Rives. "Vision-Based Automatic Approach and Landing of Fixed-Wing Aircraft Using a Dense Visual Tracking." In Informatics in Control Automation and Robotics. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-19730-7_19.

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Chen, Yonghong, Fengming Han, Chong Zhen, Xiulin Zhang, Yuxiang Zhang, and Yufeng Mi. "Order Reduction Control Design for Carrier-Based Aircraft Automatic Carrier Landing System." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-6613-2_212.

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Wang, Lipeng, Donghui Yuan, Qidan Zhu, and Zixia Wen. "Lateral Automatic Landing Control of Carrier-Based Aircraft Based on Nonlinear Dynamic Inversion." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-6613-2_59.

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Kaden, André, Bernd Boche, and Robert Luckner. "Hardware-in-the-Loop Flight Simulator – An Essential Part in the Development Process for the Automatic Flight Control System of a Utility Aircraft." In Advances in Aerospace Guidance, Navigation and Control. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38253-6_34.

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Conference papers on the topic "Aircraft - Automatic Control"

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Jones, Lim Jen Nee, Rini Akmeliawati, and Chee Pin Tan. "Automatic aircraft landing control using Nonlinear Energy Method." In Control (MSC). IEEE, 2010. http://dx.doi.org/10.1109/cca.2010.5611294.

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CRASSIDIS, JOHN, and D. MOOK. "An automatic carrier landing system utilizing aircraft sensors." In Navigation and Control Conference. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2666.

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Li, Yingchun, Hexin Chen, Yunhuan Mei, Jianbo Yang, and Wei Zheng. "Automatic aircraft object detection in aerial images." In Fifth International Symposium on Instrumentation and Control Technology, edited by Guangjun Zhang, Huijie Zhao, and Zhongyu Wang. SPIE, 2003. http://dx.doi.org/10.1117/12.521906.

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Zollitsch, Alexander W., Nils C. Mumm, Simona Wulf, et al. "Automatic takeoff of a general aviation research aircraft." In 2017 11th Asian Control Conference (ASCC). IEEE, 2017. http://dx.doi.org/10.1109/ascc.2017.8287427.

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Meng, Hao, and Yingzhen Li. "Fuzzy controller design for automatic carrier landing of aircraft." In 2014 33rd Chinese Control Conference (CCC). IEEE, 2014. http://dx.doi.org/10.1109/chicc.2014.6895687.

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Wang Min, Chen WenLiang, Lin MeiAn, Jiang HongYu, Yu Lu, and Wang YuBo. "Case study of aircraft fuselage automatic assembly simulation." In 2010 International Conference on Mechanic Automation and Control Engineering (MACE). IEEE, 2010. http://dx.doi.org/10.1109/mace.2010.5535294.

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Burlion, Laurent, Henry de Plinval, and Philippe Mouyon. "Backstepping based visual servoing for transport aircraft automatic landing." In 2014 IEEE Conference on Control Applications (CCA). IEEE, 2014. http://dx.doi.org/10.1109/cca.2014.6981530.

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Lo, C. H., Eric H. K. Fung, and Y. K. Wong. "Knowledge-Based Automatic Fault Detection in Flight Control System." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-41495.

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There are various possible failures, like, actuator, sensor, or structural, which can occur on a sophisticated modern aircraft. In certain situations the need for an automatic fault detection system provides additional information about the status of the aircraft to assist pilots to compensate for failures. In this paper, we develop an intelligent technique based on fuzzy-genetic algorithm for automatically detecting failures in flight control system. The fuzzy-genetic algorithm is proposed to construct the automatic fault detection system for monitoring aircraft behaviors. Fuzzy system is employed to estimates the times and types of actuator failure. Genetic algorithms are used to generate an optimal fuzzy rule set based on the training data. The optimization capability of genetic algorithms provides and efficient and effective way to generate optimal fuzzy rules. Different types of actuator failure can be detected by the fuzzy-genetic algorithm based automatic fault detection system after tuning its rule table. Simulations with different actuator failures of the non-linear F-16 aircraft model are conducted to appraise the performance of the proposed automatic fault detection system.
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Min, Byoung-Mun, Min-Jea Tahk, Byoung-Soo Kim, and Hyo-Sang Shin. "Guidance Law for Automatic Landing of Tilt-Rotor Aircraft." In AIAA Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-6353.

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MCINGVALE, PAT, and SHARON DUDLEY. "Expert system technology applied to the automatic control of multiple unmanned aerial vehicles." In Aircraft Design, Systems and Operations Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-3280.

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Reports on the topic "Aircraft - Automatic Control"

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H H AEROSPACE DESIGN CO INC BEDFORD MA. Advanced Air Traffic Control Concept Study: Automated Tactical Aircraft Launch and Recovery System (ATALARS). Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada229100.

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David, Aharon. Controlling Aircraft—From Humans to Autonomous Systems: The Fading Humans. SAE International, 2023. http://dx.doi.org/10.4271/epr2023014.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;While being the first to fly, the Wright Brothers were also the first and last complete “one stop shop” of aviation: the only case in human flight in which the same individuals personally carried out the research, development, testing, manufacturing, operation, maintenance, air control, flight simulation, training, setup, operation, and more. Since then, these facets gradually fragmented and drifted away from the aircraft. This report discusses the phenomenon of aircraft operation’s “fading humans,” including the development of flight instruments to support it, its growing automation, the emerging artificial intelligence paradigm, and the lurking cyber threats that all over the place.&lt;/div&gt;&lt;div class="htmlview paragraph"&gt;&lt;b&gt;Controlling Aircraft – From Humans to Autonomous Systems: The Fading Humans&lt;/b&gt; examines the “fading” process itself, including its safety aspects, current mitigation efforts, ongoing research, and the unsettled topics that still remain.&lt;/div&gt;&lt;div class="htmlview paragraph"&gt;&lt;a href="https://www.sae.org/publications/edge-research-reports" target="_blank"&gt;Click here to access the full SAE EDGE&lt;/a&gt;&lt;sup&gt;TM&lt;/sup&gt;&lt;a href="https://www.sae.org/publications/edge-research-reports" target="_blank"&gt; Research Report portfolio.&lt;/a&gt;&lt;/div&gt;&lt;/div&gt;
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