Interception of a hypersonic vehicle by low-speed interceptors: novel perspectives and cost optimisation

• Autorzy: Liu Shuangxi , Liu Shijun , Yan Binbin , Zhang Tong , Zhang Xu , Yan Jie

Identyfikatory

DOI

10.24425/bpasts.2022.143537

• Języki publikacji: EN

Abstrakty

EN

The conditions for accurately intercepting hypersonic vehicles by low-speed interceptors in the terminal guidance process are examined, considering the general form of a guidance scheme. First, based on the concept of the engagement geometry, three interception scenarios are established considering different manoeuvring configurations of the interceptors and hypersonic vehicle. Second, the boundary conditions for intercepting hypersonic vehicles (with speeds higher than those of the interceptors) are specified for the three scenarios, considering several factors: the speed, path angle, line-of-sight angle, and available overload of the interceptor; path angle and manoeuvrability of the hypersonic vehicle; and relative distance between the interceptor and vehicle. A series of simulations are performed to clarify the influence of each factor on the interception performance in the three interception scenarios. The challenges associated with accurately intercepting hypersonic vehicles by low-speed interceptors are summarised, and several recommendations for designing guidance laws are presented.

Słowa kluczowe

EN

small speed ratio; hypersonic vehicle; interception performance; boundary conditions

PL

mały współczynnik prędkości; pojazd hipersoniczny; wydajność przechwytywania; warunki brzegowe

• Wydawca: Polska Akademia Nauk, Wydział IV Nauk Technicznych
• Czasopismo: Bulletin of the Polish Academy of Sciences. Technical Sciences
• Rocznik: 2022
• Tom: Vol. 70, nr 6
• Strony: art. no. e143537
• Opis fizyczny: Bibliogr. 38 poz., rys.

Twórcy

autor

Liu Shuangxi

• Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China

• https://orcid.org/0000-0002-1422-1096

autor

Liu Shijun

• Shanghai Aerospace Equipment Manufacturer Co., Ltd, Shanghai 200245, China

autor

Yan Binbin

• School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, China

• https://orcid.org/0000-0003-1082-8808

autor

Zhang Tong

• Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China

autor

Zhang Xu

• Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China

autor

Yan Jie

• Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China

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Uwagi

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).