DE602008000222D1 - Aktive Steuerung von weichen Hybridisoliersystemen - Google Patents

Aktive Steuerung von weichen Hybridisoliersystemen

Info

Publication number
DE602008000222D1
DE602008000222D1 DE602008000222T DE602008000222T DE602008000222D1 DE 602008000222 D1 DE602008000222 D1 DE 602008000222D1 DE 602008000222 T DE602008000222 T DE 602008000222T DE 602008000222 T DE602008000222 T DE 602008000222T DE 602008000222 D1 DE602008000222 D1 DE 602008000222D1
Authority
DE
Germany
Prior art keywords
active control
insulation systems
hybrid insulation
soft hybrid
soft
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
DE602008000222T
Other languages
English (en)
Inventor
Timothy A Hindle
Brian J Hamilton
Louis R Jackson
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.)
Honeywell International Inc
Original Assignee
Honeywell International 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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of DE602008000222D1 publication Critical patent/DE602008000222D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • 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
    • 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
    • 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
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B64G1/6425—Interstage or payload connectors arrangements for damping vibrations
    • 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
    • B64G1/32—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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE602008000222T 2007-03-16 2008-01-31 Aktive Steuerung von weichen Hybridisoliersystemen Active DE602008000222D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/687,551 US7953523B2 (en) 2007-03-16 2007-03-16 Active control of soft hybrid isolation systems

Publications (1)

Publication Number Publication Date
DE602008000222D1 true DE602008000222D1 (de) 2009-12-03

Family

ID=39588028

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008000222T Active DE602008000222D1 (de) 2007-03-16 2008-01-31 Aktive Steuerung von weichen Hybridisoliersystemen

Country Status (4)

Country Link
US (1) US7953523B2 (de)
EP (1) EP1977972B1 (de)
JP (1) JP2008254726A (de)
DE (1) DE602008000222D1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100020742A1 (en) * 2008-07-24 2010-01-28 Lockheed Martin Corporation Hybrid spacecraft for communications and remote sensing
JP5591199B2 (ja) * 2011-09-14 2014-09-17 三菱電機株式会社 振動絶縁装置
US9410596B2 (en) 2011-11-04 2016-08-09 Honeywell International Inc. Mounting systems for structural members, fastening assemblies thereof, and vibration isolation systems including the same
US8678323B2 (en) * 2012-02-28 2014-03-25 Honeywell International Inc. Launch lock assemblies including axial gap amplification devices and spacecraft isolation systems including the same
US9475594B2 (en) 2012-09-25 2016-10-25 Honeywell International Inc. Launch lock assemblies with reduced preload and spacecraft isolation systems including the same
CN103984238B (zh) * 2014-06-05 2016-08-31 湖南大学 基于虚拟弹簧阻尼网络的卫星编队构形分布式控制方法
US9828117B2 (en) * 2016-02-04 2017-11-28 United Launch Alliance, L.L.C. Tensioning apparatus and system for clamping joints
EP3950512A1 (de) * 2016-05-05 2022-02-09 L'garde, Inc. Sonnensegel für orbitale manöver
CN109116730B (zh) * 2018-07-11 2021-10-12 南京航空航天大学 一种基于tu合作博弈的混合执行机构能量优化管理方法
US11321496B2 (en) 2019-01-23 2022-05-03 The Aerospace Corporation Distributed attitude control system for reconfigurable spacecraft composed of joined entities with compliant coupling
CN111332497B (zh) * 2020-03-23 2022-04-22 南京航空航天大学 一种超稳卫星平台及调姿控制方法
CN111580532B (zh) * 2020-04-28 2023-04-14 北京控制工程研究所 一种航天器多级系统的聚合分离三超控制方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848525A (en) 1987-11-02 1989-07-18 The Boeing Company Dual mode vibration isolator
US5305981A (en) 1991-10-31 1994-04-26 Honeywell Inc. Multiaxis vibration isolation system
US6022005A (en) * 1996-09-27 2000-02-08 Trw Inc. Semi-active vibration isolator and fine positioning mount
US6354576B1 (en) 1999-10-22 2002-03-12 Honeywell International Inc. Hybrid passive and active vibration isolator architecture
US6454215B1 (en) 2001-01-29 2002-09-24 Lockheed Martin Corporation Spacecraft architecture for disturbance-free payload

Also Published As

Publication number Publication date
JP2008254726A (ja) 2008-10-23
US20080228332A1 (en) 2008-09-18
US7953523B2 (en) 2011-05-31
EP1977972B1 (de) 2009-10-21
EP1977972A1 (de) 2008-10-08

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition