EA201700523A1 - DEVICE FOR ELECTRODYNAMIC CABLE SYSTEM STABILIZATION TO REMOVE SPACE GARBAGE - Google Patents

DEVICE FOR ELECTRODYNAMIC CABLE SYSTEM STABILIZATION TO REMOVE SPACE GARBAGE

Info

Publication number
EA201700523A1
EA201700523A1 EA201700523A EA201700523A EA201700523A1 EA 201700523 A1 EA201700523 A1 EA 201700523A1 EA 201700523 A EA201700523 A EA 201700523A EA 201700523 A EA201700523 A EA 201700523A EA 201700523 A1 EA201700523 A1 EA 201700523A1
Authority
EA
Eurasian Patent Office
Prior art keywords
cable
space
cable system
earth
local vertical
Prior art date
Application number
EA201700523A
Other languages
Russian (ru)
Other versions
EA035609B1 (en
Inventor
Алексей Александрович ТИХОНОВ
Original Assignee
Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный университет" (СПбГУ)
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 Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный университет" (СПбГУ) filed Critical Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный университет" (СПбГУ)
Publication of EA201700523A1 publication Critical patent/EA201700523A1/en
Publication of EA035609B1 publication Critical patent/EA035609B1/en

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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
    • B64G1/34—Guiding or controlling apparatus, e.g. for attitude control using gravity gradient

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Chemical & Material Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laying Of Electric Cables Or Lines Outside (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

Изобретение относится к космической технике и может быть использовано для стабилизации космической тросовой системы в околоземном пространстве. Для функционирования электродинамической тросовой системы в околоземном пространстве в режиме ориентации вдоль местной вертикали размещают коллекторы для сбора зарядов противоположных знаков по концам троса. При взаимодействии зарядов с магнитным полем Земли возникает момент лоренцевых сил, который оказывает ориентирующее действие на трос. Для достижения устойчивой ориентации троса вдоль местной вертикали параметры троса выбирают в соответствии с условиями, учитывающими также влияние возмущающих моментов, что позволяет при наличии демпфирования решить задачу стабилизации троса в положении вдоль местной вертикали.The invention relates to space technology and can be used to stabilize the space cable system in near-Earth space. For the operation of the electrodynamic cable system in near-earth space in the orientation mode along the local vertical, collectors are placed to collect charges of opposite signs at the ends of the cable. In the interaction of charges with the Earth’s magnetic field, a moment of Lorentz forces arises, which has an orienting effect on the cable. To achieve a stable orientation of the cable along the local vertical, the parameters of the cable are chosen in accordance with the conditions that also take into account the influence of disturbing moments, which allows, in the presence of damping, to solve the problem of stabilizing the cable in position along the local vertical.

EA201700523A 2017-08-22 2017-11-23 Device for stabilizing an electrodynamic rope system for space debris removal EA035609B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2017129790A RU2666610C1 (en) 2017-08-22 2017-08-22 Device of stabilization of electrodynamic cable system for removing space waste

Publications (2)

Publication Number Publication Date
EA201700523A1 true EA201700523A1 (en) 2019-02-28
EA035609B1 EA035609B1 (en) 2020-07-15

Family

ID=63580251

Family Applications (1)

Application Number Title Priority Date Filing Date
EA201700523A EA035609B1 (en) 2017-08-22 2017-11-23 Device for stabilizing an electrodynamic rope system for space debris removal

Country Status (2)

Country Link
EA (1) EA035609B1 (en)
RU (1) RU2666610C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2709295C1 (en) * 2018-11-16 2019-12-17 Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный университет" (СПбГУ)" Damping device for stabilization of electrodynamic rope system

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1819829A1 (en) * 1991-03-29 1993-06-07 Mo I Svyazi Method of erection of space structures on base of dynamic flexible coupling
RU2092401C1 (en) * 1995-07-05 1997-10-10 Центральный научно-исследовательский институт машиностроения Method of electrodynamic action with magnetoplasma near-planet medium and electrodynamic cable system for realization of this method
RU2159201C2 (en) * 1998-10-29 2000-11-20 Тихонов Алексей Александрович Method of control of artificial satellite orientation
US6758443B1 (en) * 2001-03-07 2004-07-06 Tether Applications, Inc. Method for observing and stabilizing electrodynamic tethers
RU2332334C1 (en) * 2006-10-24 2008-08-27 Кирилл Андреевич Антипов Method of semi-passive three-axis stabilisation of dynamically symmetric artificial earth satellite

Also Published As

Publication number Publication date
RU2666610C1 (en) 2018-09-11
EA035609B1 (en) 2020-07-15

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Legal Events

Date Code Title Description
MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AM AZ BY KZ KG TJ TM RU