Abstract
At present reusable aircraft is a research hotspot in the field of aerospace. When a high-speed re-entry vehicle re-enters the atmosphere, obtaining accurate flight parameters such as angle of attack, sideslip angle and dynamic pressure plays a crucial role in control and stability. The traditional outrigger pitot tube and attack/sideslip angle sensing system will cause a series of structural and thermal problems at high speed, and cannot be applied to high angle of attack flight conditions. In order to solve these problems, a flush air data system (FADS) was developed. FADS based on the measurement of pressure information from multiple pressure taps embedded in the surface of the fuselage, combined with the pressure distribution model to solve the atmospheric parameters. This paper studies how to verify the reliability of FADS. The correctness of the FADS algorithm is verified by laboratory tests and the adaptability of the FADS is verified by wind tunnel tests. The test results can effectively evaluate the performance of FADS.
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References
Baoguo, W.: Basics of Aerodynamics. National Defense Industry Press, Beijing (2009)
Zhiliang, L.: Aerodynamics. Beijing University of Aeronautics and Astronautics Press, Beijing (2009)
Chen, L.: Research on Embedded Atmospheric Data System Algorithms and Key Technologies of Atmospheric Data Sensing Information Fusion. Nanjing University of Aeronautics and Astronautics, Nanjing (2018)
Hairui, J.: Research on Data Estimation and Method of Embedded Atmospheric Data Sensing System. Nanjing University of Aeronautics and Astronautics, Nanjing (2017)
Yijie, D., Pengfei, P.: Research on the measurement method of atmospheric data in hypersonic flight. Tactical Missile Technol. 3, 37–40 (2013)
Nan, B., Zhaofeng, S., Jingchun, Y., et al.: Research on embedded air data sensing technology. Aeronaut. Missile 8, 79–85 (2010)
Peng, W., Xin, J., Weimin, Z.: Research on the solution accuracy of embedded air data sensing system for blunt air body. Mech. Practice 38(3), 255–261 (2016)
Lu, C., Li, R.B., Liu, J.Y.: Air data estimation by fusing navigation system and flight control system. J. Navig. 71, 1231–1246 (2018)
Keshmiri, S., Colgren, R., Mirmirani, M.: Development of an aerodynamic database for a generic hypersonic air vehicle. In: AIAA Guidance, Navigation, and Control Conference and Exhibit, San Francisco, California: AIAA, pp. 1–21 (2005)
Bibb, K.L., Cassidy, L.D., Schwing, A.M.: Orion EFT-1 FADS based trajectory reconstruction. AIAA-2016-3254 (2016)
Whitmore, S.A., Cobleigh, B.R., Hearing, E.A.: Design and calibration of the X-33 Flush Air Data Sensing (FADS) System. NASATM-206540 (1998)
Davis, M.C., Pahle, J.W., White, J.T., et al.: Development of a flush airdata sensing system on a sharp-nosed vehicle for flight at Mach 3 to 8. NASA TM-2000-209017 (2000)
Whitmore, S., Moes, T.: The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system (2013)
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Hu, S., Qi, Q., Liang, L., Guo, T. (2023). Test Verification Method of FADS Algorithm for Reusable Aircraft. In: Yan, L., Duan, H., Deng, Y. (eds) Advances in Guidance, Navigation and Control. ICGNC 2022. Lecture Notes in Electrical Engineering, vol 845. Springer, Singapore. https://doi.org/10.1007/978-981-19-6613-2_317
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DOI: https://doi.org/10.1007/978-981-19-6613-2_317
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