Patent US3489128A successfully refreshed from Google Patents.
Patent US4358767A successfully refreshed from Google Patents.
US4358767A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of tracking for telecommunications antennae
Assignee: Neyrpic SA
•
Filing: 1980-12-29
•
Granted: 1982-11-09
•
Expires: 2000-12-29
Abstract
Abstract A method of tracking for telecommunications antennae. It consists in carrying out continuous measurements along each axis (X,Y) of displacement and in returning backwards by a measured amount before proceeding to change the axis.
Inventors
- 👤 Claude Boireau
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 22:01
CPC Classifications
G; G01; G01S; G01S3/00; G01S3/02; G01S3/14; G01S3/38; G01S3/44
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
258 words
A method of tracking by antenna, characterized in controlling the driving unit (17, 18) of an antenna (16) so as to aim it in the direction of the satellite in accordance with the following steps: (a) measure the output voltage from a receiver; (b) displace the antenna along a first axis, and in a certain direction; (c) during the displacement, successively measure the output voltage and successively compare each measurement with the previous one; (d) when a measurement is found to be less than the previous one, change the direction of displacement along the same axis; (e) during the new displacement, successively measure the output voltage and successively compare each measurement with the previous one; (f) when a measurement is found to be less than the previous one, stop and then displace in the reverse direction along the same axis for a measured time t1, depending upon the driving speed of the antenna, along this axis and determined so as to be that which provides the best aim at the end of the cycle, then change the axis by 90°; (g) repeat along this orthogonal axis with another measured time t2 which is a function of the driving speed along this axis and is determined so as to be that which provides the best aim at the end of the cycle, of the steps (a) to (f) with either stopping of the tracking or repetition of a complete cycle (a) to (g), the number of cycles of this type before stopping the tracking being programmable by the user.
Claim 2
Independent Claim
258 words
A method of tracking by antenna, characterized in controlling the driving unit (17, 18) of an antenna (16) so as to aim it in the direction of the satellite in accordance with the following steps: (a) measure the output voltage from a receiver; (b) displace the antenna along a first axis, and in a certain direction; (c) during the displacement, successively measure the output voltage and successively compare each measurement with the previous one; (d) when a measurement is found to be less than the previous one, change the direction of displacement along the same axis; (e) during the new displacement, successively measure the output voltage and successively compare each measurement with the previous one; (f) when a measurement is found to be less than the previous one, stop and then displace in the reverse direction along the same axis for a measured time t1, depending upon the driving speed of the antenna, along this axis and determined so as to be that which provides the best aim at the end of the cycle, then change the axis by 90°; (g) repeat along this orthogonal axis with another measured time t2 which is a function of the driving speed along this axis and is determined so as to be that which provides the best aim at the end of the cycle, of the steps (a) to (f) with either stopping of the tracking or repetition of a complete cycle (a) to (g), the number of cycles of this type before stopping the tracking being programmable by the user.
Claim 3
Dependent Claim
67 words
A method of tracking as in claim 1, characterized in that each of the said measured times (t1 and t2) is determined by setting it equal to zero, by thereupon carrying out a cycle limited to the axis in question (X or Y) and than measuring the distance along the axis in question from the position of aim obtained, to the real known position of the satellite.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-11-08 | 1986-05-10 | 1986-11-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-11-08 | 1990-05-10 | 1990-11-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-11-08 | 1994-05-10 | 1994-11-09 | $7700.00 | Window Closed / Lapsed |