FR2960030B1 - Fusee, procede de controle d'une fusee et procede d'evaluation de fusees par compensation de pression - Google Patents

Fusee, procede de controle d'une fusee et procede d'evaluation de fusees par compensation de pression

Info

Publication number
FR2960030B1
FR2960030B1 FR1154032A FR1154032A FR2960030B1 FR 2960030 B1 FR2960030 B1 FR 2960030B1 FR 1154032 A FR1154032 A FR 1154032A FR 1154032 A FR1154032 A FR 1154032A FR 2960030 B1 FR2960030 B1 FR 2960030B1
Authority
FR
France
Prior art keywords
rocket
rocker
evaluating
rods
controlling
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
FR1154032A
Other languages
English (en)
Other versions
FR2960030A1 (fr
Inventor
Sean S Stroud
Michael J Piovoso
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NORTHROP GRUMMAN INNOVATION SYSTEMS, INC., US
Original Assignee
Alliant Techsystems Inc
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 Alliant Techsystems Inc filed Critical Alliant Techsystems Inc
Publication of FR2960030A1 publication Critical patent/FR2960030A1/fr
Application granted granted Critical
Publication of FR2960030B1 publication Critical patent/FR2960030B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F02K9/58—Propellant feed valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/20—Special functions
    • F05D2200/23—Logarithm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/20—Special functions
    • F05D2200/24—Special functions exponential
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/12—Purpose of the control system to maintain desired vehicle trajectory parameters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/13—Purpose of the control system to control two or more engines simultaneously
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/70—Type of control algorithm
    • F05D2270/701—Type of control algorithm proportional

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Feedback Control In General (AREA)
FR1154032A 2010-05-11 2011-05-10 Fusee, procede de controle d'une fusee et procede d'evaluation de fusees par compensation de pression Active FR2960030B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/777,508 US9677504B2 (en) 2010-05-11 2010-05-11 Rockets, methods of rocket control and methods of rocket evaluation utilizing pressure compensation

Publications (2)

Publication Number Publication Date
FR2960030A1 FR2960030A1 (fr) 2011-11-18
FR2960030B1 true FR2960030B1 (fr) 2017-02-17

Family

ID=44203162

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1154032A Active FR2960030B1 (fr) 2010-05-11 2011-05-10 Fusee, procede de controle d'une fusee et procede d'evaluation de fusees par compensation de pression

Country Status (5)

Country Link
US (1) US9677504B2 (fr)
JP (1) JP5843471B2 (fr)
FR (1) FR2960030B1 (fr)
GB (1) GB2480365B (fr)
IL (1) IL212669A (fr)

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JP5860705B2 (ja) * 2011-06-24 2016-02-16 株式会社Ｉｈｉエアロスペース パルスロケットモータ
JP6000091B2 (ja) 2012-11-27 2016-09-28 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
JP2014105657A (ja) 2012-11-28 2014-06-09 Mitsubishi Heavy Ind Ltd 軌道姿勢制御装置、軌道姿勢制御方法
JP6008713B2 (ja) * 2012-11-28 2016-10-19 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
KR101357617B1 (ko) 2013-01-16 2014-02-03 한국항공우주연구원 액체 추진체를 사용하는 로켓용 터보펌프 엔진의 압력 보정 방법
US9650996B2 (en) * 2015-03-13 2017-05-16 The Boeing Company Valve controller for pressure stabilization
RU2622427C2 (ru) * 2015-07-06 2017-06-19 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Способ управления угловым движением ракеты космического назначения
FR3042227B1 (fr) * 2015-10-08 2020-04-03 Arianegroup Sas Procede et circuit de regulation de moteur-fusee
CN109858150B (zh) * 2019-01-31 2023-02-03 北京航天发射技术研究所 复杂发射技术条件的燃气流场网格模型生成方法
CN111997784B (zh) * 2020-08-11 2021-06-22 西安航天动力试验技术研究所 一种同压力源多路并联推进剂流量精确控制装置及方法
CN112228250B (zh) * 2020-09-10 2023-06-09 沈阳航天新光集团有限公司 一种液体姿控发动机集成块
CN112989559B (zh) * 2021-01-19 2023-10-20 中国人民解放军63921部队 一种液体运载火箭体系贡献率的分析评估方法
CN112528423B (zh) * 2021-02-18 2021-04-27 中国人民解放军国防科技大学 固体火箭发动机燃面数据修正方法、装置和设备
US20230249847A1 (en) * 2022-02-10 2023-08-10 Brian Haney Methods and Device for Autonomous Rocketry
CN116579245B (zh) * 2023-05-16 2024-05-14 中国兵器装备集团自动化研究所有限公司 一种药柱密度预测方法及装置

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Also Published As

Publication number Publication date
JP2011236903A (ja) 2011-11-24
IL212669A0 (en) 2011-07-31
GB2480365A (en) 2011-11-16
US9677504B2 (en) 2017-06-13
JP5843471B2 (ja) 2016-01-13
FR2960030A1 (fr) 2011-11-18
IL212669A (en) 2014-11-30
GB2480365B (en) 2016-06-08
GB201107444D0 (en) 2011-06-15
US20110277446A1 (en) 2011-11-17

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