JPS6452598A - Tetherd satellite system - Google Patents

Tetherd satellite system

Info

Publication number
JPS6452598A
JPS6452598A JP62205000A JP20500087A JPS6452598A JP S6452598 A JPS6452598 A JP S6452598A JP 62205000 A JP62205000 A JP 62205000A JP 20500087 A JP20500087 A JP 20500087A JP S6452598 A JPS6452598 A JP S6452598A
Authority
JP
Japan
Prior art keywords
satellite
tether
satellites
navigation body
satellite system
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.)
Granted
Application number
JP62205000A
Other languages
Japanese (ja)
Other versions
JP2510614B2 (en
Inventor
Masayuki Takasaki
Kazunori Kawasaki
Koichiro Koyama
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co 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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP62205000A priority Critical patent/JP2510614B2/en
Publication of JPS6452598A publication Critical patent/JPS6452598A/en
Application granted granted Critical
Publication of JP2510614B2 publication Critical patent/JP2510614B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Measuring Magnetic Variables (AREA)

Abstract

PURPOSE: To perform observation at the respective designated altitudes at the same time by providing a tether with plural satellites in a tethered satellite system in which a satellite is connected to the tip of a tether extended from a navigation body on an earth orbit. CONSTITUTION: This tethered satellite system is so constructed that a first satellite 3 for observing rarefied air and radiation in an aerosphere is connected to the tip 2a of a tether 2 extended from a navigation body 1 toward the earth E, and the tether 2 for connecting the navigation body 1 and the first satellite 3 to each other is provided with second and third satellites 4, 5 for performing the same observation as that of the first satellite 3. The respective satellites 3-5 are sequentially connected and fixed to the satellite holding part 1a previously provided at the base of the navigation body 1 through a connecting means 6 which can be released according to a command signal. At a designated altitude, the connecting means 6 is released to sequentially lower the satellites by gas injection, etc., of a thruster 3a provided on the first satellite 3 and position the same the respective designated altitudes.
JP62205000A 1987-08-20 1987-08-20 Tethered satellite system Expired - Lifetime JP2510614B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP62205000A JP2510614B2 (en) 1987-08-20 1987-08-20 Tethered satellite system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62205000A JP2510614B2 (en) 1987-08-20 1987-08-20 Tethered satellite system

Publications (2)

Publication Number Publication Date
JPS6452598A true JPS6452598A (en) 1989-02-28
JP2510614B2 JP2510614B2 (en) 1996-06-26

Family

ID=16499791

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62205000A Expired - Lifetime JP2510614B2 (en) 1987-08-20 1987-08-20 Tethered satellite system

Country Status (1)

Country Link
JP (1) JP2510614B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106855690A (en) * 2016-11-24 2017-06-16 西北工业大学 Robot of space rope system reclaims the self-adaptation control method of target after closely arresting

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4097010A (en) * 1975-10-08 1978-06-27 Smithsonian Institution Satellite connected by means of a long tether to a powered spacecraft
JPS5822799A (en) * 1981-08-03 1983-02-10 三菱電機株式会社 Control system for mass characteristic of artificial satellite

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4097010A (en) * 1975-10-08 1978-06-27 Smithsonian Institution Satellite connected by means of a long tether to a powered spacecraft
JPS5822799A (en) * 1981-08-03 1983-02-10 三菱電機株式会社 Control system for mass characteristic of artificial satellite

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106855690A (en) * 2016-11-24 2017-06-16 西北工业大学 Robot of space rope system reclaims the self-adaptation control method of target after closely arresting
CN106855690B (en) * 2016-11-24 2020-04-03 西北工业大学 Self-adaptive control method for recovering target after space tethered robot short-distance capture

Also Published As

Publication number Publication date
JP2510614B2 (en) 1996-06-26

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