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Статті в журналах з теми "090104 Aircraft Performance and Flight Control Systems"
Fielding, C., and M. Lodge. "Stability and control of STOVL aircraft: The design of longitudinal flight control laws." Aeronautical Journal 104, no. 1038 (August 2000): 383–89. http://dx.doi.org/10.1017/s0001924000064022.
Повний текст джерелаLandy, R. J., W. A. Yonke, and J. F. Stewart. "Development of HIDEC Adaptive Engine Control Systems." Journal of Engineering for Gas Turbines and Power 109, no. 2 (April 1, 1987): 146–51. http://dx.doi.org/10.1115/1.3240017.
Повний текст джерелаKöthe, Alexander, and Robert Luckner. "Applying Eigenstructure Assignment to Inner-Loop Flight Control Laws for a Multibody Aircraft." CEAS Aeronautical Journal 13, no. 1 (December 21, 2021): 33–43. http://dx.doi.org/10.1007/s13272-021-00549-z.
Повний текст джерелаSTEPAN, Anca, Georges GHAZI, and Ruxandra Mihaela BOTEZ. "Development of an Adaptive Aero-Propulsive Performance Model in Cruise Flight – Application to the Cessna Citation X." INCAS BULLETIN 14, no. 4 (December 2, 2022): 167–81. http://dx.doi.org/10.13111/2066-8201.2022.14.4.14.
Повний текст джерелаTromboni, Pier Domenico, and Giovanni B. Palmerini. "Navigation Aids Performance Evaluation for Precision Approaches." International Journal of Aerospace Engineering 2010 (2010): 1–10. http://dx.doi.org/10.1155/2010/389832.
Повний текст джерелаLee, A. W., and J. K. Hedrick. "Application of Approximate I/O Linearization to Aircraft Flight Control." Journal of Dynamic Systems, Measurement, and Control 116, no. 3 (September 1, 1994): 429–36. http://dx.doi.org/10.1115/1.2899238.
Повний текст джерелаRay, A., and J. Caplin. "Life extending control of aircraft: trade-off between flight performance and structural durability." Aeronautical Journal 104, no. 1039 (September 2000): 397–408. http://dx.doi.org/10.1017/s0001924000091843.
Повний текст джерелаIyaghigba, Samuel David, Fakhre Ali, and Ian K. Jennions. "A Review of Diagnostic Methods for Hydraulically Powered Flight Control Actuation Systems." Machines 11, no. 2 (January 25, 2023): 165. http://dx.doi.org/10.3390/machines11020165.
Повний текст джерелаShim, Jong-Ik. "Improving Aircraft Database Performance for Flight Simulator." International Review of Aerospace Engineering (IREASE) 14, no. 1 (February 28, 2021): 28. http://dx.doi.org/10.15866/irease.v14i1.19310.
Повний текст джерелаHuang, Min, Zhong-wei Wang, Xing-Bao Yang, Zhen-yun Guo, and Yao-bin Niu. "Preliminary Validation of the Wind Tunnel Based Flight Control System Evaluation Method." MATEC Web of Conferences 179 (2018): 03021. http://dx.doi.org/10.1051/matecconf/201817903021.
Повний текст джерелаДисертації з теми "090104 Aircraft Performance and Flight Control Systems"
Collins, David C. (David Charles) 1969. "Adaptive model reference control of highly maneuverable high performance aircraft." Thesis, 1993. http://hdl.handle.net/1957/37416.
Повний текст джерелаGraduation date: 1993
(9762536), Shupeng Liu. "Sustainable Autonomous Solar UAV with Distributed Propulsion System." Thesis, 2021.
Знайти повний текст джерелаSolar-powered Unmanned Aerial Vehicles (UAVs) solve the problem of loiter time as aircrafts can fly as long as sufficient illumination and reserve battery power is available. However, Solar-powered UAVs still face the problem of excessive wingspan to increase solar capture area, which detracts from maneuverability and portability. As a result, a feature of merit for solar UAVs has emerged that strives to reduce the wingspan of such UAVs. The purpose of this project is to improve energy use efficiency by applying a distributed propulsion system to reduce the wingspan of solar-powered UAVs and increase payload. The research focuses on optimizing a new design analysis method applied to the distributed propulsion system and further employs the novel application of solar arrays on both top and bottom of the wings. The design methodology will result in a 2.1-meter wingspan, which is the shortest at 2020, for a 24-hour duration solar-powered UAV.
(8063924), Austin L. Nash. "Hierarchical Combined Plant and Control Design for Thermal Management Systems." Thesis, 2019.
Знайти повний текст джерелаIn this thesis, I develop a new design approach for TMSs called hierarchical control co-design (HCCD). More specifically, I develop a HCCD algorithm aimed at optimizing high-fidelity design and control for a TMS across a system hierarchy. This is accomplished in part by integrating system level (SL) CCD with detailed component level (CL) design optimization. The lower-fidelity SL CCD algorithm incorporates feedback control into the design of a TMS to ensure controllability and robust transient response to exogenous disturbances, and the higher-fidelity CL design optimization algorithms provide a way of designing detailed components to achieve the desired performance needed at the SL. Key specifications are passed back and forth between levels of the hierarchy at each iteration to converge on an optimal design that is responsive to desired objectives at each level. The resulting HCCD algorithm permits the design and control of a TMS that is not only optimized for steady-state efficiency, but that can be designed for robustness to transient disturbances while achieving said disturbance rejection with minimal compromise to system efficiency. Several case studies are used to demonstrate the utility of the algorithm in designing systems with different objectives. Additionally, high-fidelity thermal modeling software is used to validate a solution to the proposed model-based design process.
Книги з теми "090104 Aircraft Performance and Flight Control Systems"
Navarro, Robert. Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Знайти повний текст джерелаNavarro, Robert. Performance of an electro-hydrostatic actuator on the F-18 systems research aircraft. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1997.
Знайти повний текст джерелаMurphy, Patrick C. Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаC, Murphy Patrick. Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаC, Murphy Patrick. Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft. [Washington, D.C: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаFranklin, James A. Moving-base simulation evaluation of control/display integration issues for ASTOVL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Знайти повний текст джерелаFranklin, James A. Moving-base simulation evaluation of control/display integration issues for ASTOVL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Знайти повний текст джерелаFranklin, James A. Moving-base simulation evaluation of control/display integration issues for ASTOVL aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.
Знайти повний текст джерелаSchmidt, D. K. Cooperative control theory and integrated flight and propulsion control: Final technical report for grant NAG3-575 covering the period 1994-1995. College Park, Md: Dept. of Aerospace Engineering, University of Maryland, 1995.
Знайти повний текст джерелаMaine, Trindel A. A preliminary evaluation of an F100 engine parameter estimation process using flight data. Moffett Field, Calif: Ames Research Center, 1990.
Знайти повний текст джерелаЧастини книг з теми "090104 Aircraft Performance and Flight Control Systems"
Kemer, Emre, Hasan Başak, and Hayri Baytan Özmen. "Performance Improvement for Fighter Aircraft Using Fuzzy Switching LQI Controller." In Fuzzy Control Systems [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.107032.
Повний текст джерелаТези доповідей конференцій з теми "090104 Aircraft Performance and Flight Control Systems"
CHIN, J., V. CHACON, and J. GERA. "X-29A flight control system performance during flight test." In Aircraft Design, Systems and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2878.
Повний текст джерелаRice, Caleb, Yu Gu, Haiyang Chao, Trenton Larrabee, Srikanth Gururajan, Marcello Napolitano, Tanmay Mandal, and Matthew Rhudy. "Control performance analysis for autonomous close formation flight experiments." In 2014 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2014. http://dx.doi.org/10.1109/icuas.2014.6842372.
Повний текст джерелаKim, Hyeongseok, Daejin Lim, and Kwanjung Yee. "Flight Control Simulation and Battery Performance Analysis of a Quadrotor under Wind Gust." In 2020 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2020. http://dx.doi.org/10.1109/icuas48674.2020.9214058.
Повний текст джерелаPORTER, B., A. MANGANAS, and T. MANGANAS. "Design of digital model-following flight-mode control systems for high-performance aircraft." In Guidance, Navigation and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4116.
Повний текст джерелаHair, Kenneth A. "Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft." In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1987. http://dx.doi.org/10.4271/871875.
Повний текст джерелаPORTER, B., and M. OTHMAN. "Design of adaptive digital model-following flight-mode control systems for high-performance aircraft." In Guidance, Navigation and Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-3495.
Повний текст джерелаWu, Falin, Jiaqi He, Guopeng Zhou, Haolun Li, and Yushuang Liu. "Performance of Sliding Mode and Consensus-based Control Approaches for Quadrotor Leader-Follower Formation Flight." In 2021 International Conference on Unmanned Aircraft Systems (ICUAS). IEEE, 2021. http://dx.doi.org/10.1109/icuas51884.2021.9476782.
Повний текст джерела"Synthesis of a reduced order model and design of a multivariable flight control system for a high performance helicopter." In Aircraft Design, Systems and Operations Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4501.
Повний текст джерелаPORTER, B., and T. MANGANAS. "Design of fast non-interacting digital flight-mode control systems for high-performance aircraft." In 7th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1903.
Повний текст джерелаMoguel, Israel, Hever Moncayo, Andres Perez, Mario Perhinschi, Dia Al Azzawi, and Adil Togayev. "Bio-Inspired Approach for Aircraft Health Assessment and Flight Envelope Estimation." In ASME 2014 Dynamic Systems and Control Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/dscc2014-5885.
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