DE69603246T2 - Optimales System zum Ändern der Lage der Solarpanelen - Google Patents

Optimales System zum Ändern der Lage der Solarpanelen

Info

Publication number
DE69603246T2
DE69603246T2 DE69603246T DE69603246T DE69603246T2 DE 69603246 T2 DE69603246 T2 DE 69603246T2 DE 69603246 T DE69603246 T DE 69603246T DE 69603246 T DE69603246 T DE 69603246T DE 69603246 T2 DE69603246 T2 DE 69603246T2
Authority
DE
Germany
Prior art keywords
changing
solar panels
optimal system
optimal
solar
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.)
Expired - Lifetime
Application number
DE69603246T
Other languages
English (en)
Other versions
DE69603246D1 (de
Inventor
John R Murphy
Ross Crowley
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Publication of DE69603246D1 publication Critical patent/DE69603246D1/de
Application granted granted Critical
Publication of DE69603246T2 publication Critical patent/DE69603246T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • B64G1/36—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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/407—Solar sailing
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • 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
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
    • B64G1/24—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
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Sustainable Energy (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE69603246T 1995-12-22 1996-12-18 Optimales System zum Ändern der Lage der Solarpanelen Expired - Lifetime DE69603246T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/577,436 US5816540A (en) 1995-12-22 1995-12-22 Optimal solar tracking system

Publications (2)

Publication Number Publication Date
DE69603246D1 DE69603246D1 (de) 1999-08-19
DE69603246T2 true DE69603246T2 (de) 2000-03-16

Family

ID=24308721

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69603246T Expired - Lifetime DE69603246T2 (de) 1995-12-22 1996-12-18 Optimales System zum Ändern der Lage der Solarpanelen

Country Status (3)

Country Link
US (1) US5816540A (de)
EP (1) EP0780296B1 (de)
DE (1) DE69603246T2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5996942A (en) * 1996-10-16 1999-12-07 Space Systems/Loral, Inc. Autonomous solar torque management
US6003817A (en) * 1996-11-12 1999-12-21 Motorola, Inc. Actively controlled thermal panel and method therefor
FR2765190B1 (fr) * 1997-06-26 1999-08-27 Aerospatiale Satellite a rejet thermique ameliore
US6076774A (en) * 1998-08-12 2000-06-20 Hughes Electronics Corporation Fuel and thermal optimal spiral earth acquisition
US6019320A (en) * 1998-09-15 2000-02-01 Hughes Electronics Corporation Spacecraft acquisition of sun pointing
FR2789653B1 (fr) * 1999-02-16 2001-04-13 Matra Marconi Space France Satellite a generateur solaire sur bras depliable et procede de mise a poste d'un tel satellite
US6311929B1 (en) * 1999-11-26 2001-11-06 Space Systems/Loral, Inc. Spacecraft and appendage stepping methods that improve spacecraft attitude pointing and cancel solar array slew disturbances
DE10114085C1 (de) * 2001-03-22 2002-07-25 Astrium Gmbh Verfahren zum Betrieb eines rotierenden Raumfahrzeugs mit variierender Rotation
FR2823182B1 (fr) * 2001-04-05 2004-06-04 Cit Alcatel Radiateur deployable pour engin spatial
US6883757B2 (en) * 2002-10-09 2005-04-26 Lockheed Martin Corporation System and method for increasing the roll offset operating range for a spacecraft
US6990396B2 (en) * 2002-12-13 2006-01-24 The Boeing Company Method and apparatus for reaction wheel dynamic compensation in long-duration deployment of a large reflector
US7025307B2 (en) * 2002-12-13 2006-04-11 The Boeing Company Method and apparatus for solar tacking momentum maintenance in long-duration deployment of a large reflector
US20050241691A1 (en) * 2004-01-10 2005-11-03 Wakefield Glenn M Space Construction
US8260944B2 (en) * 2007-09-07 2012-09-04 International Business Machines Corporation Using a state machine embedded within a session initiation protocol (SIP) servlet to implement an application programming interface (API)
US8868263B2 (en) 2011-05-25 2014-10-21 Space Systems/Loral, Llc Spacecraft momentum management using solar array
FR2980176A1 (fr) * 2011-09-19 2013-03-22 Astrium Sas Procede de controle d'attitude d'un satellite et satellite commande en attitude
FR2996526B1 (fr) * 2012-10-05 2015-05-15 Thales Sa Satellite a modules de charge utile deployables
US20150367968A1 (en) * 2014-06-19 2015-12-24 Honeywell International Inc. Systems and methods for a momentum platform
US10259599B2 (en) * 2015-12-08 2019-04-16 Space Systems/Loral, Llc Spacecraft with rigid antenna reflector deployed via linear extension boom
RU2706643C2 (ru) * 2016-08-19 2019-11-19 Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ контроля производительности солнечной батареи космического аппарата с инерционными исполнительными органами
CN109032158B (zh) * 2018-07-24 2021-07-09 北京控制工程研究所 一种直线规划的头对日—尾对日交替连续偏航姿态控制方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4325124A (en) 1979-02-28 1982-04-13 Organisation Europeenne De Recherches Spatiales System for controlling the direction of the momentum vector of a geosynchronous satellite
FR2513589A1 (fr) * 1981-09-28 1983-04-01 Aerospatiale Procede et dispositif pour aligner l'axe de roulis d'un satellite avec une direction desiree
DE3329955A1 (de) * 1983-08-19 1985-03-07 Erno Raumfahrttechnik Gmbh, 2800 Bremen Lageregelung von satelliten
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
FR2656586B1 (fr) * 1989-12-29 1992-05-07 Aerospatiale Dispositif de controle d'attitude par voiles solaires pour satellite stabilise autour de trois axes.
US5337981A (en) * 1991-11-27 1994-08-16 Hughes Aircraft Company Method and apparatus for compensating for solar torque transients on a satellite during a solar eclipse
CA2080613A1 (en) * 1991-11-27 1993-05-28 Douglas J. Bender Method and apparatus for dynamic precompensation of solar wing stepping motions of a satellite
US5310144A (en) * 1992-07-06 1994-05-10 Hughes Aircraft Company Method and apparatus for satellite torque balancing
US5305971A (en) * 1992-07-14 1994-04-26 Trw Inc. Spacecraft control by electrochromic devices

Also Published As

Publication number Publication date
DE69603246D1 (de) 1999-08-19
US5816540A (en) 1998-10-06
EP0780296A1 (de) 1997-06-25
EP0780296B1 (de) 1999-07-14

Similar Documents

Publication Publication Date Title
DE69603246D1 (de) Optimales System zum Ändern der Lage der Solarpanelen
DE19681316T1 (de) System zum Erweitern der Ziehfunktion
DE69616283D1 (de) Pflanzeinheit
DE69316260D1 (de) Energieversorgungssystem
NO980112D0 (no) Hastighets-kontroller
DE69521172D1 (de) Anlagenbetriebsunterstützungssystem
FR2756945B1 (fr) Navigation solaire multiaxiale
FI971901A0 (fi) Konstruktioelementti rakenteita varten
ATA76192A (de) Solaranlage
ATA59393A (de) Sonnenkollektor
ATA41992A (de) Sonnenkollektor
KR970006116A (ko) 동체구조
ES1030404Y (es) Soporte para paneles de cultivo.
KR970018973U (ko) 태양열의 집열판
SE9502846D0 (sv) Solfångare
KR960035948U (ko) 집란장치
KR950015554U (ko) 수상관용 프레임 구조
SE9200408D0 (sv) Luftare foer raavatten
KR940018721U (ko) 식물 지지대
BR9502717A (pt) Eletroionizador solar para água
NO940708D0 (no) Solvarmesystem
FR2726888B1 (fr) Structures de modules etoiles
BR9500304A (pt) Lemes de superficie rigidos horizontais
NO973115D0 (no) Solfölgesystem for solcellepaneler
BR7200329U (pt) Regulador de painel solar - rps/tolhc

Legal Events

Date Code Title Description
8364 No opposition during term of opposition