EA201890077A2 - Способы и устройства для минимизации динамики выдачи команд для спутника - Google Patents

Способы и устройства для минимизации динамики выдачи команд для спутника

Info

Publication number
EA201890077A2
EA201890077A2 EA201890077A EA201890077A EA201890077A2 EA 201890077 A2 EA201890077 A2 EA 201890077A2 EA 201890077 A EA201890077 A EA 201890077A EA 201890077 A EA201890077 A EA 201890077A EA 201890077 A2 EA201890077 A2 EA 201890077A2
Authority
EA
Eurasian Patent Office
Prior art keywords
vectors
dynamics
satellite
devices
issuing commands
Prior art date
Application number
EA201890077A
Other languages
English (en)
Other versions
EA039190B1 (ru
EA201890077A3 (ru
Inventor
Тимоти С. Луи
Гари И. Лемке
Original Assignee
Зе Боинг Компани
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 Зе Боинг Компани filed Critical Зе Боинг Компани
Publication of EA201890077A2 publication Critical patent/EA201890077A2/ru
Publication of EA201890077A3 publication Critical patent/EA201890077A3/ru
Publication of EA039190B1 publication Critical patent/EA039190B1/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/413—Ion or plasma engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Plasma & Fusion (AREA)

Abstract

Раскрыты способы, устройства и изделие для минимизации динамики выдачи команд для спутника. Приведенное в качестве примера устройство включает в себя модуль законов управления для вычисления первого набора векторов для маневрирования космического аппарата и вычисления второго набора векторов на основании проецирования первого набора векторов на фиксированную плоскость. Устройство дополнительно включает в себя контроллер пространственного положения для выработки команды пространственного положения на основании первого и второго наборов векторов для предотвращения незапланированного поворота космического аппарата.
EA201890077A 2017-03-22 2018-01-16 Способы и устройства для минимизации динамики выдачи команд для спутника EA039190B1 (ru)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/466,228 US10175700B2 (en) 2017-03-22 2017-03-22 Methods and apparatus to minimize command dynamics of a satellite

Publications (3)

Publication Number Publication Date
EA201890077A2 true EA201890077A2 (ru) 2018-09-28
EA201890077A3 EA201890077A3 (ru) 2018-11-30
EA039190B1 EA039190B1 (ru) 2021-12-15

Family

ID=61132139

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201890077A EA039190B1 (ru) 2017-03-22 2018-01-16 Способы и устройства для минимизации динамики выдачи команд для спутника

Country Status (6)

Country Link
US (1) US10175700B2 (ru)
EP (1) EP3379366B1 (ru)
JP (1) JP7084168B2 (ru)
CN (1) CN108627158B (ru)
CA (1) CA2991997C (ru)
EA (1) EA039190B1 (ru)

Cited By (1)

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CN111498150A (zh) * 2020-03-27 2020-08-07 中国科学院西安光学精密机械研究所 一种星载大惯量旋转载荷角动量和力矩补偿方法及系统

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US10291316B1 (en) * 2017-12-11 2019-05-14 Star Mesh LLC Data transmission systems and methods using satellite-to-satellite radio links
CN111319791B (zh) * 2020-02-28 2021-10-01 上海航天控制技术研究所 一种适用于火星探测的姿态控制模式管理方法
CN112109924A (zh) * 2020-08-21 2020-12-22 北京控制工程研究所 一种三维矢量方向的阵列式微阴极放电推进系统
US12227309B2 (en) * 2021-02-19 2025-02-18 Mitsubishi Electric Corporation Method for forming unified satellite constellation, unified data library, and unified satellite constellation
CN113306747B (zh) * 2021-04-27 2022-12-20 上海卫星工程研究所 基于so(3)群的挠性航天器姿态稳定控制方法和系统
CN113734468B (zh) * 2021-08-30 2023-02-03 北京宇航系统工程研究所 一种基于迭代制导的轨道面精确控制方法
CN114684388B (zh) * 2022-03-15 2025-04-29 中国科学院微小卫星创新研究院 一种基于轨道系太阳矢量实现星上自主任务规划的方法
WO2024186574A1 (en) * 2023-03-03 2024-09-12 The Board Of Trustees Of The University Of Illinois Object design using multifunctional structures for attitude control

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111498150A (zh) * 2020-03-27 2020-08-07 中国科学院西安光学精密机械研究所 一种星载大惯量旋转载荷角动量和力矩补偿方法及系统

Also Published As

Publication number Publication date
CN108627158B (zh) 2023-10-27
CA2991997C (en) 2023-05-16
CN108627158A (zh) 2018-10-09
US10175700B2 (en) 2019-01-08
JP2018184159A (ja) 2018-11-22
EA039190B1 (ru) 2021-12-15
CA2991997A1 (en) 2018-09-22
EP3379366A1 (en) 2018-09-26
EP3379366B1 (en) 2024-04-10
US20180275683A1 (en) 2018-09-27
EA201890077A3 (ru) 2018-11-30
JP7084168B2 (ja) 2022-06-14

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