GB1424383A - Tpower systems for spacecraft or orbiting satellites - Google Patents

Tpower systems for spacecraft or orbiting satellites

Info

Publication number
GB1424383A
GB1424383A GB3129473A GB3129473A GB1424383A GB 1424383 A GB1424383 A GB 1424383A GB 3129473 A GB3129473 A GB 3129473A GB 3129473 A GB3129473 A GB 3129473A GB 1424383 A GB1424383 A GB 1424383A
Authority
GB
United Kingdom
Prior art keywords
regulator
section
bus leads
spacecraft
systems
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
Application number
GB3129473A
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics Ltd
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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Priority to GB3129473A priority Critical patent/GB1424383A/en
Priority to BE147307A priority patent/BE818510A/en
Priority to NL7410720A priority patent/NL7410720A/en
Priority to DK424774A priority patent/DK424774A/da
Priority to FR7427709A priority patent/FR2240148B3/fr
Priority to DE2438919A priority patent/DE2438919A1/en
Publication of GB1424383A publication Critical patent/GB1424383A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05FSYSTEMS FOR REGULATING ELECTRIC OR MAGNETIC VARIABLES
    • G05F1/00Automatic systems in which deviations of an electric quantity from one or more predetermined values are detected at the output of the system and fed back to a device within the system to restore the detected quantity to its predetermined value or values, i.e. retroactive systems
    • G05F1/10Regulating voltage or current
    • G05F1/46Regulating voltage or current wherein the variable actually regulated by the final control device is dc
    • G05F1/62Regulating voltage or current wherein the variable actually regulated by the final control device is dc using bucking or boosting dc sources
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • Y02E10/56Power conversion systems, e.g. maximum power point trackers

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Photovoltaic Devices (AREA)
  • Control Of Electrical Variables (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

1424383 Supply systems for spacecrafts or satellites HAWKER SIDDELEY DYNAMICS Ltd 6 Aug 1974 [11 Aug 1973] 31294/73 Heading H2H A power supply system for an orbiting spacecraft or satellite comprises a solar array having sections 12a, 12b, 12c which are switchable into and out of circuit across main bus leads 16 by a control logic circuit 17 of a voltage regulator and an array section 12 connected to the bus leads via a fine control section 21 of the regulator, and a battery 14 provided with a charge control regulator 13. In sunlight, the power supply is regulated by the control logic circuit 17 which controls the closure of switches 19a, 19b, 19c and by the fine section 21 of the regulator which controls the supplementary power supplied by the array section 12. During eclipse, the battery 14 supplies power to the bus leads via the regulator section 21.
GB3129473A 1973-08-11 1973-08-11 Tpower systems for spacecraft or orbiting satellites Expired GB1424383A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB3129473A GB1424383A (en) 1973-08-11 1973-08-11 Tpower systems for spacecraft or orbiting satellites
BE147307A BE818510A (en) 1973-08-11 1974-08-05 IMPROVEMENT OF THE ENERGY SYSTEM OF AN ORBITAL SPACE MACHINE
NL7410720A NL7410720A (en) 1973-08-11 1974-08-09 CONTROL EQUIPMENT FOR THE POWER SUPPLY OF A SPACE VESSEL FOR MAINTAINING SATELLITES IN A PARTICULAR PATH.
DK424774A DK424774A (en) 1973-08-11 1974-08-09
FR7427709A FR2240148B3 (en) 1973-08-11 1974-08-09
DE2438919A DE2438919A1 (en) 1973-08-11 1974-08-10 POWER SUPPLY SYSTEM FOR A CIRCULATING SPACESHIP OR A SATELLITE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3129473A GB1424383A (en) 1973-08-11 1973-08-11 Tpower systems for spacecraft or orbiting satellites

Publications (1)

Publication Number Publication Date
GB1424383A true GB1424383A (en) 1976-02-11

Family

ID=10320995

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3129473A Expired GB1424383A (en) 1973-08-11 1973-08-11 Tpower systems for spacecraft or orbiting satellites

Country Status (6)

Country Link
BE (1) BE818510A (en)
DE (1) DE2438919A1 (en)
DK (1) DK424774A (en)
FR (1) FR2240148B3 (en)
GB (1) GB1424383A (en)
NL (1) NL7410720A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4243928A (en) * 1979-05-29 1981-01-06 Exxon Research & Engineering Co. Voltage regulator for variant light intensity photovoltaic recharging of secondary batteries
EP0051959A1 (en) * 1980-10-31 1982-05-19 Solarex Corporation Voltage regulator for photovoltaic charging systems
GB2132837A (en) * 1982-12-23 1984-07-11 Rca Corp Satellite power distribution system
GB2166306A (en) * 1984-10-26 1986-04-30 Aurora Mechatronics Corp Solar-energised computer
EP1160876A2 (en) * 2000-05-30 2001-12-05 The Boeing Company Reconfigurable solar module array
US10225953B2 (en) 2014-10-31 2019-03-05 Thermal Corp. Vehicle thermal management system
CN110824269A (en) * 2019-09-26 2020-02-21 中国空间技术研究院 Power supply and distribution joint test verification system and method based on comprehensive electronic system
CN113612253A (en) * 2021-08-06 2021-11-05 北京空间飞行器总体设计部 High-voltage bus spacecraft power grid-connected control device
CN113725987A (en) * 2021-08-26 2021-11-30 绵阳天仪空间科技有限公司 Novel commercial satellite power supply system
CN113791663A (en) * 2021-07-19 2021-12-14 北京空间飞行器总体设计部 High-power spacecraft power supply system based on solar cell array maximum power point tracking technology

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE439405B (en) * 1980-12-17 1985-06-10 Jungner Ab Nife METHOD OF CHARGING AN ELECTRIC ACCUMULATOR BATTERY BY SOLAR PANELS CONTAINING SOLAR CELLS, AND DEVICE FOR CHARGING ACCORDING TO THE METHOD
DE3146701A1 (en) * 1981-11-25 1983-07-07 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Arrangement for voltage regulation of a power supply system for space vehicles
FR2521361A1 (en) * 1982-02-09 1983-08-12 Photowatt Int BATTERY CHARGE REGULATOR

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4243928A (en) * 1979-05-29 1981-01-06 Exxon Research & Engineering Co. Voltage regulator for variant light intensity photovoltaic recharging of secondary batteries
EP0051959A1 (en) * 1980-10-31 1982-05-19 Solarex Corporation Voltage regulator for photovoltaic charging systems
GB2132837A (en) * 1982-12-23 1984-07-11 Rca Corp Satellite power distribution system
GB2166306A (en) * 1984-10-26 1986-04-30 Aurora Mechatronics Corp Solar-energised computer
EP1160876A2 (en) * 2000-05-30 2001-12-05 The Boeing Company Reconfigurable solar module array
EP1160876A3 (en) * 2000-05-30 2006-10-04 The Boeing Company Reconfigurable solar module array
US10225953B2 (en) 2014-10-31 2019-03-05 Thermal Corp. Vehicle thermal management system
US10932392B2 (en) 2014-10-31 2021-02-23 Aavid Thermal Corp. Vehicle thermal management system
CN110824269A (en) * 2019-09-26 2020-02-21 中国空间技术研究院 Power supply and distribution joint test verification system and method based on comprehensive electronic system
CN113791663A (en) * 2021-07-19 2021-12-14 北京空间飞行器总体设计部 High-power spacecraft power supply system based on solar cell array maximum power point tracking technology
CN113612253A (en) * 2021-08-06 2021-11-05 北京空间飞行器总体设计部 High-voltage bus spacecraft power grid-connected control device
CN113612253B (en) * 2021-08-06 2024-02-09 北京空间飞行器总体设计部 High-voltage bus spacecraft power grid-connected control device
CN113725987A (en) * 2021-08-26 2021-11-30 绵阳天仪空间科技有限公司 Novel commercial satellite power supply system

Also Published As

Publication number Publication date
DE2438919A1 (en) 1975-02-20
DK424774A (en) 1975-04-14
NL7410720A (en) 1975-02-13
BE818510A (en) 1974-12-02
FR2240148A1 (en) 1975-03-07
FR2240148B3 (en) 1977-06-10

Similar Documents

Publication Publication Date Title
GB1424383A (en) Tpower systems for spacecraft or orbiting satellites
US4494063A (en) Satellite dual bus power system
US20170305579A1 (en) Power architecture for solar electric propulsion applications
GB1034694A (en) Improvements relating to power supplies in satellites
RUSCIO The San Marco D/L power system design(aeronomical satellite)
DENZINGER et al. Rosat's power subsystem
BOEHRINGER et al. Dynamic behaviour of power conditioning systems for satellites with a maximum-power-point-tracking system(Behavior of satellite power conditioning systems emphasizing maximum-power-point tracking)
GB979969A (en) Improvements relating to battery installations for vehicles or aircraft
CAPEL et al. A sequenced PWM controlled power conditioning unit for a regulated bus satellite power system(Sequenced PWM controlled power conditioning unit for regulated bus satellite power system)
JPS6426335A (en) Power supply system
Ghosh et al. Achievement of synchronous orbit using electric propulsion
IT1251918B (en) POWER SUPPLY AND CONTROL DEVICE PARTICULARLY FOR IONIC RADIOFREQUENCY PREPULSERS.
HOLDAWAY et al. Optimisation of geostationary satellite emplacement by low thrust propulsion(Geostationary satellite trajectory optimization by low thrust resistojet propulsion)
BREDIUS The power system of the Astronomical Netherlands Satellite(Power supply system of Astronomical Netherlands Satellite noting converters, regulators and batteries)
PAULKOVICH Solar bus regulator and battery charger for IMP's H, I, and J(Service life of IMP H, I, and J power systems controlled by solar bus regulator and battery charger)
ANDREWS Power conditioning equipment for a thermoelectric outer planet spacecraft, volume 1, book 1(Design and development of power conditioning equipment for TOPS spacecraft for outer planets missions)[Final Technical Report, Apr. 1969- Dec. 1971]
SU847438A1 (en) Self-sustained electric power supply system
Dunlop Communications satellite power conditioning systems
Hajela et al. Start-up capabilities of photovoltaic module for the International Space Station
Raab et al. Solar vs. nuclear power-Is there a choice
Bechtel et al. Thrust vector control using electric actuation
HOEGSHOLM Design aspects of the PCU for the GEOS power system(satellite power control unit)
MacKenzie et al. Nimbus Power Systems (1960-1969)
Clermont et al. Wheel Energy Storage Systems for satellite power conditioning and attitude control
POTIN Optimization of PWM power units(Optimization of PWM power regulating units)

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee