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US4038528A Expired / Lapsed US ⏱️ 0.0 years remaining

Automatic piloting system

Assignee: Laitram LLC
•
Filing: 1975-11-10
•
Granted: 1977-07-26
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Expires: 1995-11-10
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Abstract

Abstract An automatic piloting system for the automatic steering of a marine or other vessel along an intended course in which a digital signal representing an intended course is processed to provide rudder commands for steering the desired course.

Inventors

  • 👤 John T. Fowler

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 03:17
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/02; G05D1/0206

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 169 words
An automatic piloting system comprising: a digital magnetic compass providing a digital output signal representative of magnetic compass heading; digital means operative in response to said compass output signal to produce a course error signal representative of the difference between said compass heading and a desired course heading; means operative in response to said course error signal to provide first and second signals representative of the integral and the derivative of course error, respectively; rudder angle means operative to provide a signal representative of the present angular position of the rudder; means for combining said first signal, said second signal, and said course error signal and for providing a control signal representative of the difference between the combined signal and said signal from said rudder angle means; means defining a range of output signals within which no rudder control is provided; and output gate means operative in response to said control signal and said range defining means for providing rudder control signals representing course errors outside of said range.
Claim 2
Dependent Claim 169 words
An automatic piloting system comprising: a digital magnetic compass providing a digital output signal representative of magnetic compass heading; digital means operative in response to said compass output signal to produce a course error signal representative of the difference between said compass heading and a desired course heading; means operative in response to said course error signal to provide first and second signals representative of the integral and the derivative of course error, respectively; rudder angle means operative to provide a signal representative of the present angular position of the rudder; means for combining said first signal, said second signal, and said course error signal and for providing a control signal representative of the difference between the combined signal and said signal from said rudder angle means; means defining a range of output signals within which no rudder control is provided; and output gate means operative in response to said control signal and said range defining means for providing rudder control signals representing course errors outside of said range.
Claim 3
Dependent Claim 33 words
The automatic piloting system of claim 1 further including: means defining a second range of control signals within which said rudder control signals are provided and outside of which rudder control is inhibited.
Claim 4
Dependent Claim 60 words
The automatic piloting system of claim 1 wherein said range defining means includes: first comparator means having a positive relative reference threshold; second comparator means having a negative relative reference threshold; said first and second comparator means being operative to provide an output signal in response to a received control signal respectively greater or less than the associated reference threshold.
Claim 5
Dependent Claim 59 words
The automatic piloting system of claim 3 including: pulse generating means operative to receive output signals from said first and second comparator means and to provide output pulse signals in response to comparator output signals of magnitude less than a predetermined level, and DC output signals in response to comparator output signals of magnitude greater than said predetermined level.
Claim 6
Dependent Claim 58 words
The automatic piloting system of claim 3 wherein said digital means includes: a course error circuit operative in response to said digital signal representation from said magnetic compass and having means for storing a representation of a desired course heading, said course error circuit providing intermediate digital output signals representative of the magnitude and sense of course error.
Claim 7
Dependent Claim 67 words
The automatic piloting system of claim 1 wherein said rudder angle means includes: a rudder angle indicator coupled to a rudder to be controlled and operative to provide a pulse width modulated signal representative of the angular position of said rudder; demodulator means operative in response to said pulse width modulated signal to provide an output signal of magnitude representative of the angular position of said rudder.

References Cited (Backward Citations)

US3280781A Cited
US3358633A Cited
US3596163A Cited
US3761791A Cited
US3949696A Cited
US3772503A Cited
US3919961A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-07-25 1981-01-24 1981-07-26 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-07-25 1985-01-24 1985-07-26 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-07-25 1989-01-24 1989-07-26 $7700.00 Window Closed / Lapsed

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