JPS5225399A - System for determining attitude and orbit of manmade satellite - Google Patents
System for determining attitude and orbit of manmade satelliteInfo
- Publication number
- JPS5225399A JPS5225399A JP50099949A JP9994975A JPS5225399A JP S5225399 A JPS5225399 A JP S5225399A JP 50099949 A JP50099949 A JP 50099949A JP 9994975 A JP9994975 A JP 9994975A JP S5225399 A JPS5225399 A JP S5225399A
- Authority
- JP
- Japan
- Prior art keywords
- orbit
- satellite
- determining attitude
- manmade
- manmade satellite
- 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.)
- Pending
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
- B64G1/242—Orbits and trajectories
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Navigation (AREA)
Abstract
PURPOSE: To provide a system for determining six elements of distance between the center of the earth and the center of the satellite, attitude of the satellite and orbit by means of a plurality of earth sensors and sun sensors mounted on a man-made satellite.
COPYRIGHT: (C)1977,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP50099949A JPS5225399A (en) | 1975-08-18 | 1975-08-18 | System for determining attitude and orbit of manmade satellite |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP50099949A JPS5225399A (en) | 1975-08-18 | 1975-08-18 | System for determining attitude and orbit of manmade satellite |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5225399A true JPS5225399A (en) | 1977-02-25 |
Family
ID=14260944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP50099949A Pending JPS5225399A (en) | 1975-08-18 | 1975-08-18 | System for determining attitude and orbit of manmade satellite |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5225399A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS548400A (en) * | 1977-06-20 | 1979-01-22 | Mitsubishi Electric Corp | System of controlling attitude of triple spindle control satellite |
JPH02130417A (en) * | 1988-11-10 | 1990-05-18 | Nec Corp | Inter-planet navigator |
CN108639385A (en) * | 2018-05-15 | 2018-10-12 | 浙江大学 | A kind of implementation method of the most simple posture control system fast and stable control of no benchmark |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3521835A (en) * | 1967-06-05 | 1970-07-28 | Massachusetts Inst Technology | Synchronous satellite |
-
1975
- 1975-08-18 JP JP50099949A patent/JPS5225399A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3521835A (en) * | 1967-06-05 | 1970-07-28 | Massachusetts Inst Technology | Synchronous satellite |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS548400A (en) * | 1977-06-20 | 1979-01-22 | Mitsubishi Electric Corp | System of controlling attitude of triple spindle control satellite |
JPH02130417A (en) * | 1988-11-10 | 1990-05-18 | Nec Corp | Inter-planet navigator |
CN108639385A (en) * | 2018-05-15 | 2018-10-12 | 浙江大学 | A kind of implementation method of the most simple posture control system fast and stable control of no benchmark |
CN108639385B (en) * | 2018-05-15 | 2021-04-13 | 浙江大学 | Method for realizing rapid and stable control of non-reference simplest attitude control system |
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