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특허 상세정보

Orbit attitude control device, and method of controlling orbit attitude

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/26    G05D-001/08   
출원번호 US-0018683 (2013-09-05)
등록번호 US-9302790 (2016-04-05)
우선권정보 JP-2012-260151 (2012-11-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Wenderoth, Lind & Ponack, L.L.P.
인용정보 피인용 횟수 : 0  인용 특허 : 17
초록

An orbit attitude control device includes a plurality of nozzles for injecting combustion gas supplied from a combustion chamber, and a control section configured to calculate nozzle opening degree correction values so that a deviation between a detection value of the pressure of the combustion chamber and a command value becomes smaller. The control section is configured to calculate a total correction value so that the deviation between the detection value and the command values becomes smaller. A total value T1 for first group nozzles and a total valu...

대표
청구항

1. An orbit attitude control device, comprising: a plurality of nozzles configured to inject combustion gas supplied from a combustion chamber, in which opening degrees are configured to be controlled in accordance with opening degree command values; anda control section configured to calculate nozzle opening degree correction values that are correction values for opening degree command values so that a deviation between a detection value of a pressure of the combustion chamber and a command value of the pressure becomes smaller to correct the opening de...

이 특허에 인용된 특허 (17)

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