Patent US4647932A successfully refreshed from Google Patents.
US4647932A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Spacecraft velocity measurement system
Assignee: NEC Corp
•
Filing: 1983-04-25
•
Granted: 1987-03-03
•
Expires: 2003-04-25
Abstract
Abstract A system for measuring the velocity of a spacecraft from a position onboard the spacecraft is disclosed. This system includes a radio wave receiver means for receiving pulse trains from a plurality of preselected pulsars. A velocity measuring unit located on the spacecraft measures the velocity of the spacecraft based on the Doppler shift of the pulse trains transmitted from each of the plurality of preselected pulsars.
Inventors
- 👤 Takesi Ono
- 👤 Kazuo Nakamura
- 👤 Toshio Okamoto
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 19:39
CPC Classifications
G; G01; G01S; G01S11/00; G01S11/02; G01S11/10
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
133 words
A system for measuring the directional velocity of a spacecraft onboard the spacecraft, the system comprising: a radio wave receiver means located on the spacecraft for receiving pulse trains from at least three preselected pulsars; frequency counter means responsive to the output of said receiver means for measuring the pulse repetition period of a respective pulse train from each of said pulsars; memory means for storing predetermined information about the pulse repetition period of the pulse train transmitted from each of said pulsars, which information is previously measured and calculated on the earth; and control means for detecting the Doppler shifts of said received pulse trains to compute the velocity vector of the spacecraft by utilizing the pulse repetition periods measured by said frequency counter means and said information in said memory means.
Claim 2
Independent Claim
133 words
A system for measuring the directional velocity of a spacecraft onboard the spacecraft, the system comprising: a radio wave receiver means located on the spacecraft for receiving pulse trains from at least three preselected pulsars; frequency counter means responsive to the output of said receiver means for measuring the pulse repetition period of a respective pulse train from each of said pulsars; memory means for storing predetermined information about the pulse repetition period of the pulse train transmitted from each of said pulsars, which information is previously measured and calculated on the earth; and control means for detecting the Doppler shifts of said received pulse trains to compute the velocity vector of the spacecraft by utilizing the pulse repetition periods measured by said frequency counter means and said information in said memory means.
Claim 3
Dependent Claim
84 words
A system according to claim 1, wherein said receiver means receives the pulse trains transmitted from each of said pulsars and produces a corresponding pulse signal representative of said pulse trains, said receiver means being responsive to a control signal which adjusts said receiver means to an optimum state for receiving of the respective pulse train transmitted by each of said pulsars; and wherein said control means provides said control signal to said receiver means in accordance with said information in said memory means.
Claim 4
Dependent Claim
19 words
A system according to claim 2, wherein said control means computes said velocity vector by the least square method.
Claim 5
Dependent Claim
179 words
A system according to claim 2, wherein said receiver means comprises: an antenna of variable directivity for receiving the respective pulse trains transmitted from said plurality of pulsars; an antenna driver for selectively controlling the direction of said antenna in response to an antenna direction control signal; a frequency converter for converting the frequency of each pulse train received by said antenna by using a local oscillation signal; a local oscillator responsive to a local oscillation frequency control signal and for supplying said frequency converter with a signal having a frequency corresponding to the frequency of each of the pulse trains from said plurality of pulsars as said local oscillation signal; and a detector for detecting each pulse train from said frequency converter and shaping the waveform of the detected pulse train thereby providing a signal which corresponds to the output of the receiver means, said control means providing said antenna direction control signal and said local oscillation frequency control signal each as a component of said control signal on the basis of said information in said memory means.
Claim 6
Independent Claim
17 words
A system according to claims 2, 3 or 4, wherein said memory means comprises a read-only memory.
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) | 1990-03-02 | 1990-09-01 | 1991-03-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-02 | 1994-09-01 | 1995-03-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-02 | 1998-09-01 | 1999-03-03 | $7700.00 | Window Closed / Lapsed |