Research on the application of high-speed flight vehicles for testing aerospace electronics
17 viewsDOI:
https://doi.org/10.54939/1859-1043.j.mst.FEE.2024.184-190Keywords:
Dynamics; Structures; Flight vehicles.Abstract
In this study, the authors conducted calculations and testing of a high-speed flight vehicle, designated as TLM-515. TLM-515 achieved a peak velocity of approximately 750 m/s and a maximum altitude of around 10 km. The vehicle carried two critical, self-developed electronic devices: a GPS satellite navigation device and an inertial navigation sensor (INS), collectively referred to as onboard systems. The objective was to evaluate their independent and combined operational capabilities in high-speed flight conditions. Test results demonstrated that TLM-515 followed a stable trajectory, and the onboard systems effectively measured the vehicle's kinematic parameters, thereby assessing the functionality of the electronics in a high-speed environment. This solution has shown a high level of reliability, suggesting its potential applicability to similar experimental platforms.
References
[1]. American Institute of Aeronautics and Astronautics, “Guide to Reference and Standard Atmosphere Models”, Reston, VA: AIAA, (2010).
[2]. “MTCR Guidelines and the Equipment, Software and Technology Annex”, (2021). [Online]. Available: https://mtcr.info/guidelines-for-sensitive-goods/
[3]. Nguyen, D.T., et al. "Trajectory and Performance Analysis of High-Altitude Sounding Rockets with INS and GPS Integration." Aerospace Science and Technology Journal, Volume 118, Issue 4, pp. 456-472, (2022).
[4]. Smith, J., et al. "In-Flight Validation of GPS-INS Systems on High-Speed Vehicles." Journal of Guidance, Control, and Dynamics, Volume 44, Issue 3, pp. 689-703, (2021).
[5]. А. Т.П.,Толкачева И.О. “Баллистическое проектирование ЛА”. Издательство МГТУ, (1990).
[6]. Кашин В.М., Лифиц А.Л., Ефремов М.И. “Основы проектирования переносных зенитных ракетных комплексов”. Москва, Изд-во МГТУ им. Н. Э. Баумана, (2014).
