UA126618U - SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING - Google Patents

SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING

Info

Publication number
UA126618U
UA126618U UAU201801142U UAU201801142U UA126618U UA 126618 U UA126618 U UA 126618U UA U201801142 U UAU201801142 U UA U201801142U UA U201801142 U UAU201801142 U UA U201801142U UA 126618 U UA126618 U UA 126618U
Authority
UA
Ukraine
Prior art keywords
aircraft
landing
gasodynamic
automatic stabilization
connection
Prior art date
Application number
UAU201801142U
Other languages
Ukrainian (uk)
Inventor
Микола Федорович Тупіцин
Ілля Олександрович Степаненко
Сергій Олександрович Малахов
Ігор Сергійович Швалюк
Original Assignee
Микола Федорович Тупіцин
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Микола Федорович Тупіцин filed Critical Микола Федорович Тупіцин
Priority to UAU201801142U priority Critical patent/UA126618U/en
Publication of UA126618U publication Critical patent/UA126618U/en

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  • Mobile Radio Communication Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Система автоматичної стабілізації літального апарата (ЛА) при його газодинамічному зльоті і посадці складається з несучої платформи, блока управління, наземної радіоапаратури. Система додатково містить блок датчиків положення ЛА відносно несучої платформи, що з'єднаний з наземною радіоапаратурою, триступеневий блок кутового положення ЛА з датчиками крену, рискання і тангажа, який розміщений на ЛА і з'єднаний з пристроєм радіозв'язку. Кожна з газодинамічних установок: основна та допоміжна, має матричну структуру, причому кожний елемент матриці має незалежне від інших джерело повітряного струменя.The system of automatic stabilization of the aircraft (LA) at its gas-dynamic take-off and landing consists of a carrier platform, a control unit, terrestrial radio equipment. The system additionally contains a block of sensors position LA relative to the carrier platform connected to the terrestrial radio, a three-stage block angular position LA with sensors roll, yaw and pitch, which is located on the LA and connected to the radio device. Each of the gas-dynamic installations: the main and auxiliary, has a matrix structure, and each element of the matrix has an independent source of air jet.

UAU201801142U 2018-02-06 2018-02-06 SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING UA126618U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201801142U UA126618U (en) 2018-02-06 2018-02-06 SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201801142U UA126618U (en) 2018-02-06 2018-02-06 SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING

Publications (1)

Publication Number Publication Date
UA126618U true UA126618U (en) 2018-06-25

Family

ID=62781717

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201801142U UA126618U (en) 2018-02-06 2018-02-06 SYSTEM OF AUTOMATIC STABILIZATION OF AIRCRAFT AT ITS GASODYNAMIC CONNECTION AND LANDING

Country Status (1)

Country Link
UA (1) UA126618U (en)

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