RU2019100549A3 - - Google Patents

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Publication number
RU2019100549A3
RU2019100549A3 RU2019100549A RU2019100549A RU2019100549A3 RU 2019100549 A3 RU2019100549 A3 RU 2019100549A3 RU 2019100549 A RU2019100549 A RU 2019100549A RU 2019100549 A RU2019100549 A RU 2019100549A RU 2019100549 A3 RU2019100549 A3 RU 2019100549A3
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RU
Russia
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RU2019100549A
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Russian (ru)
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RU2019100549A (en
RU2730814C2 (en
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RU2019100549A 2019-01-14 2019-01-14 Method for intelligent information support of helicopter crew on altitude and speed parameters and parameters of air environment surrounding helicopter, and device for implementation thereof RU2730814C2 (en)

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Application Number Priority Date Filing Date Title
RU2019100549A RU2730814C2 (en) 2019-01-14 2019-01-14 Method for intelligent information support of helicopter crew on altitude and speed parameters and parameters of air environment surrounding helicopter, and device for implementation thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2019100549A RU2730814C2 (en) 2019-01-14 2019-01-14 Method for intelligent information support of helicopter crew on altitude and speed parameters and parameters of air environment surrounding helicopter, and device for implementation thereof

Publications (3)

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RU2019100549A RU2019100549A (en) 2020-07-15
RU2019100549A3 true RU2019100549A3 (en) 2020-07-15
RU2730814C2 RU2730814C2 (en) 2020-08-26

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RU2019100549A RU2730814C2 (en) 2019-01-14 2019-01-14 Method for intelligent information support of helicopter crew on altitude and speed parameters and parameters of air environment surrounding helicopter, and device for implementation thereof

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Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112052427B (en) * 2020-09-25 2024-04-02 中国直升机设计研究所 Helicopter warship surface free parking stability calculation method
RU2757939C1 (en) * 2020-12-29 2021-10-25 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Method for assessing the spatial position of a helicopter-type aircraft
RU2771577C1 (en) * 2021-07-30 2022-05-05 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Helicopter avionics complex
CN115933803B (en) * 2023-01-09 2023-06-13 江苏东成工具科技有限公司 Equipment control method, equipment and computer readable medium
CN116629026B (en) * 2023-07-18 2023-09-26 中国海洋大学 BP neural network-based vortex nuclear underwater maximum temperature anomaly inversion method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2427844C1 (en) * 2010-03-09 2011-08-27 Государственное образовательное учреждение высшего профессионального образования Казанский государственный технический университет им. А.Н. Туполева Helicopter air data system
US10101356B2 (en) * 2014-02-19 2018-10-16 Eit Llc Instrument and method for measuring low indicated air speed
RU2592705C2 (en) * 2014-12-10 2016-07-27 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" Onboard system for measuring parameters of wind velocity vector during parking, takeoff and landing of helicopter
RU2651315C1 (en) * 2016-12-21 2018-04-19 Акционерное общество "Научно-производственный комплекс "ЭЛАРА" имени Г.А. Ильенко" (АО "ЭЛАРА") Helicopter air data system

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RU2019100549A (en) 2020-07-15
RU2730814C2 (en) 2020-08-26

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20210115