US4161780A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Spin rate timing system
Assignee: United States Department of the Navy
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Filing: 1978-06-23
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Granted: 1979-07-17
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Expires: 1998-06-23
Abstract
Abstract Apparatus for use in determining the orientation of a spinning spacecraft d for controlling the attitude motion thereof. In response to commands from an external processor, the apparatus enables a selected thruster at a commanded time delay after a solar-or earth-sensor reference pulse and fires the thruster a commanded number of times. The time difference between various sensor inputs is measured to determine spin rate and other data which is used by the external processor in calculating the firing sequence of the thrusters.
Inventors
- 👤 Louis R. Rudolph
- 👤 II Woodrow W. Ewen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 23:38
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/24; B64G1/36; B64G1/365; B64G1/244; B64G1/363
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
341 words
Apparatus for use in controlling the attitude of a spinning spacecraft, said apparatus receiving serial data words from an external processor and pulse inputs from sensors disposed on the spacecraft and transmitting data to said processor and signals to control thruster jets on said spacecraft, said apparatus comprising: a select shift register having its input coupled to said processor for receiving a select data word; a delay shift register having its input coupled to said processor for receiving a delay data word; a storage register having its data input coupled to the data output of said selected shift register for storing said select data word; a delay counter having its input coupled to the data output of said delay shift register; a clock coupled to said delay counter for stepping down the count in said counter; a first decoder coupled to the data output of said storage register, said first decoder receiving at least two data bits from said storage register to direct a signal received at its input to one of a plurality of outputs, said outputs controlling said thruster jets; a firing pulse counter coupled to the data output of said storage register, said firing pulse counter receiving a plurality of data bits from said storage register to enter an initial count in said counter, the delay data word loading the data in said counter; a second decoder coupled to the data output of said storage register, said second decoder receiving at least two data bits from said storage register to select one of a plurality of sensor inputs as the output of said decoder; said output being coupled to said delay counter to load the delay word in said delay shift register into said delay counter; and a one-shot multivibrator coupled to said delay counter, said multivibrator being triggered when the count in said delay counter reaches zero, the output of said multivibrator being coupled to said firing-pulse counter to step down the count in said firing-pulse counter and being coupled to the input of said first decoder.
Claim 2
Dependent Claim
341 words
Apparatus for use in controlling the attitude of a spinning spacecraft, said apparatus receiving serial data words from an external processor and pulse inputs from sensors disposed on the spacecraft and transmitting data to said processor and signals to control thruster jets on said spacecraft, said apparatus comprising: a select shift register having its input coupled to said processor for receiving a select data word; a delay shift register having its input coupled to said processor for receiving a delay data word; a storage register having its data input coupled to the data output of said selected shift register for storing said select data word; a delay counter having its input coupled to the data output of said delay shift register; a clock coupled to said delay counter for stepping down the count in said counter; a first decoder coupled to the data output of said storage register, said first decoder receiving at least two data bits from said storage register to direct a signal received at its input to one of a plurality of outputs, said outputs controlling said thruster jets; a firing pulse counter coupled to the data output of said storage register, said firing pulse counter receiving a plurality of data bits from said storage register to enter an initial count in said counter, the delay data word loading the data in said counter; a second decoder coupled to the data output of said storage register, said second decoder receiving at least two data bits from said storage register to select one of a plurality of sensor inputs as the output of said decoder; said output being coupled to said delay counter to load the delay word in said delay shift register into said delay counter; and a one-shot multivibrator coupled to said delay counter, said multivibrator being triggered when the count in said delay counter reaches zero, the output of said multivibrator being coupled to said firing-pulse counter to step down the count in said firing-pulse counter and being coupled to the input of said first decoder.
Claim 3
Dependent Claim
212 words
The apparatus as recited in claim 1 further comprising: a multiplexer coupled to the data output of said storage register, said multiplexer receiving at least two data bits from said storage register to select one of a plurality of sensor inputs as the output of said multiplexer; a first NAND gate having a first input coupled to the output of said multiplexer and a second input coupled to the data output of said storage register for receiving a data bit from said storage register; a spin-rate flip-flop having its clear input coupled to the output of said NAND gate and a toggle input coupled to a sensor input; a second NAND gate having a first input coupled to the Q output of said flip-flop and its second input coupled to said clock; a third counter having its input coupled to the output of said second NAND gate; a second storage register coupled to the data output of said third counter, the output of said second storage register being coupled to said processor; and a delay device having its input coupled to the Q output of said flip-flop, the output of said delay device loading the count in said third counter into said second storage register and resetting said third counter to zero.
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) | 1982-07-16 | 1983-01-15 | 1983-07-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-07-16 | 1987-01-15 | 1987-07-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-07-16 | 1991-01-15 | 1991-07-17 | $7700.00 | Window Closed / Lapsed |