GB2015292B - Method for determining the attitude of a spinning spacecraft - Google Patents
Method for determining the attitude of a spinning spacecraftInfo
- Publication number
- GB2015292B GB2015292B GB7906941A GB7906941A GB2015292B GB 2015292 B GB2015292 B GB 2015292B GB 7906941 A GB7906941 A GB 7906941A GB 7906941 A GB7906941 A GB 7906941A GB 2015292 B GB2015292 B GB 2015292B
- Authority
- GB
- United Kingdom
- Prior art keywords
- attitude
- determining
- spinning spacecraft
- spacecraft
- spinning
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/08—Systems for determining direction or position line
- G01S1/38—Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna
- G01S1/40—Systems for determining direction or position line using comparison of [1] the phase of the envelope of the change of frequency, due to Doppler effect, of the signal transmitted by an antenna moving, or appearing to move, in a cyclic path with [2] the phase of a reference signal, the frequency of this reference signal being synchronised with that of the cyclic movement, or apparent cyclic movement, of the antenna the apparent movement of the antenna being produced by cyclic sequential energisation of fixed antennas
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/0247—Determining attitude
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/08—Position of single direction-finder fixed by determining direction of a plurality of spaced sources of known location
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Navigation (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7906941A GB2015292B (en) | 1977-11-30 | 1979-02-27 | Method for determining the attitude of a spinning spacecraft |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4973877 | 1977-11-30 | ||
GB7906941A GB2015292B (en) | 1977-11-30 | 1979-02-27 | Method for determining the attitude of a spinning spacecraft |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2015292A GB2015292A (en) | 1979-09-05 |
GB2015292B true GB2015292B (en) | 1982-06-23 |
Family
ID=26266534
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7906941A Expired GB2015292B (en) | 1977-11-30 | 1979-02-27 | Method for determining the attitude of a spinning spacecraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2015292B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4883244A (en) * | 1987-12-23 | 1989-11-28 | Hughes Aircraft Company | Satellite attitude determination and control system with agile beam sensing |
-
1979
- 1979-02-27 GB GB7906941A patent/GB2015292B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB2015292A (en) | 1979-09-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GR64125B (en) | Method for the preparation of 3-de-o-methylfortimicins | |
GB8301030D0 (en) | Fabricated method | |
GB2040450B (en) | Gyroscope apparatus | |
GB2000315B (en) | Method for the preparation of a photothermographic system | |
DE3064962D1 (en) | Gyroscope apparatus | |
GR58448B (en) | Method for the construction of one thread-core | |
JPS5530693A (en) | Acceleration detector | |
GB2050851B (en) | Method for the recovery of acetone | |
JPS5451165A (en) | Attitude controller | |
GB2015292B (en) | Method for determining the attitude of a spinning spacecraft | |
DE2964281D1 (en) | Gyroscopes | |
PT67796A (en) | Method of making packages slip-proof | |
JPS5630606A (en) | Gyroscope | |
JPS54164144A (en) | Photooglasssfiber fixing method | |
ZW22580A1 (en) | A method of erecting a structure which includes the steps of locating structural leements | |
JPS53121042A (en) | Electrostatic coating method | |
GB2004369B (en) | Navigation aid | |
ZA784536B (en) | A method for the preparation of apovincamine from vincamine and epivincamine | |
JPS52137130A (en) | Method of fixing member | |
JPS5350770A (en) | Time indication method | |
GB2007847B (en) | Nuclear gyroscopes | |
GB2029573B (en) | Gyros | |
JPS5578209A (en) | Gyro apparatus | |
JPS55131910A (en) | Pushhbutton structure for watch | |
ZA802425B (en) | Pedometers |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |