Dual channel signal selection and fault detection system

• US 4,916,612 A
• Filed: 11/02/1987
• Issued: 04/10/1990
• Est. Priority Date: 11/02/1987
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hess, Richard W., Chin, Richard H., Maeshiro, Asamitsu
• Primary Examiner(s): Lall, Parshotam S.
• Assistant Examiner(s): Black, Thomas G.
• Application Number:
  US07/115,853
• Time in Patent Office: 890 Days
• Field of Search: 364/424.01, 364/447, 364/428, 318/564, 371/68, 371/36, 244/194, 244/184, 244/183
• US Class Current: 701/3
• CPC Class Codes: G05B 9/03 with multiple-channel loop, i.e. redundant control systems

Abstract

A signal selection and fault detection system that provides triple functional redundancy using the outputs (Y_A, Y_B) of two unmonitored primary channels and the output of one or the other of two complementary filters (22, 34) that each receive and process a signal (Y dot IRU) that is derived from a third, independent primary signal source (18) and that is representative of the rate or first derivative of the primary signals (Y_A, Y_B). During non-failure conditions, the system output (Y_CF1) is generated by a normal mode complementary filter 22 from the synthesized rate signal (Y dot IRU) and the selected (10) midvalue one of this output signal (Y_CF1) and the primary signals (Y_A, Y_B). In the event of a suspected failure in one of the primary signals, the output (Y_IRU) of a failure mode complementary filter is substituted (16) for the system output signal (Y_CF1) as the third input (C) to the midvalue selector (10). The system includes a fault monitor (24) and a fault detector (26) to monitor the selected signal and generate switching signals (LOC FAIL, IC FILT, SELCHA, SELCHB) that control the switching between the normal mode and failure mode complementary filters and the isolation of the failed channels. Provisions (30, 32) are made for initializing integrators (52, 54) in the failure mode complementary filter and for varying the band width (C1, C2, A1, A2) of both the failure mode and the normal mode complementary filters as a function of a parameter that influences the primary signals.

Claims

1. An aircraft signal selection and fault detection system, comprising:

a midvalue selector having an output and first, second, and third inputs, said first and second inputs being connected to receive first and second redundant localizer signals that are representative of the deviation of an aircraft from a runway centerline, said third input being connected to receive a third input signal that is representative of said deviation, said midvalue selector producing at its output the input signal corresponding to the midvalue of said input signals;

means for producing a synthesized rate signal that is representative of the rate of deviation of the aircraft from said runway centerline;

a normal mode complementary filter connected to receive said synthesized rate signal and the output of said midvalue selector, said filter being responsive to said signals to produce a normal mode complementary filter output signal that is representative of said deviation; and

means for coupling said normal mode complementary filter output signal as the third input signal to said midvalue selector.

2. The system of claim 1, wherein said means for producing a synthesized rate signal comprises:

an IRS midvalue selector connected to receive three redundant inertial reference signals, said IRS midvalue selector producing a midvalue inertial reference signal that is the midvalue one of said inertial reference signals; and

computation means responsive to said midvalue inertial reference signal for producing said synthesized rate signal.

3. The system of claim 2, wherein:

said midvalue inertial reference signal includes a ground speed component representative of the ground speed of an aircraft along a flight path and an angular component representative of the angular deviation of an aircraft from a desired course; and

said computation means includes means for computing a track angle error signal from said angular component and means for generating said synthesized rate signal by multiplying said ground speed component by the sine of said track angle signal.

4. A signal and fault detection system, comprising:

a midvalue sector having an output and first, second, and third inputs, said first and second inputs being connected to receive first and second redundant input signals, respectively, that correspond to a condition, said condition varying in accordance with a parameter, said third input being connected to receive a third input signal that is representative of said condition, said midvalue selector producing at its output the input signal corresponding to the midvalue of said input signals;

means for producing a condition rate signal that is representative of the rate of change of said condition;

a normal mode complementary filter connected to receive said condition rate signal and the output of said midvalue selector, said filter being responsive to said signals to produce a normal mode complementary filter output signal that is representative of said condition, said filter having a bandpass that varies in a predetermined manner as a function of said parameter; and

means for coupling said normal mode complementary filter output signal as the third input signal to said midvalue selector.

5. A signal selection and fault detection system, comprising:

a midvalue selector having an output and first, second, and third inputs, said first and second inputs being connected to receive first and second redundant input signals, respectively, that correspond to a condition, said third input being connected to receive a third input signal that is representative of said condition, said midvalue selector producing at its output the input signal corresponding to the midvalue of said input signals;

means for producing a condition rate signal that is representative of the rate of change of said condition;

a normal mode complementary filter connected to receive said condition rate signal and the output of said midvalue selector, said filter being responsive to said signals to produce a normal mode complementary filter output signal that is representative of said condition;

failure detection means for monitoring said redundant input signals and for providing a suspected failure signal when the difference between said redundant input signals exceeds a first predetermined threshold;

a failure mode complementary filter connected to receive said condition rate signal, said filter producing a failure mode complementary filter output signal that is representative of said condition; and

means for coupling said normal mode complementary filter output signal as the third input signal to said midvalue selector, said means for coupling including means responsive to said suspected failure signal for substituting said failure mode complementary filter output signal for said normal mode complementary filter output signal as the third input signal to said midvalue selector.

6. The system of claim 5, wherein said condition comprises a condition that varies in accordance with a parameter and wherein said failure mode complementary filter has a bandpass that varies in a predetermined manner as a function of said parameter.

7. The system of claim 6, wherein said normal mode complementary filter has a bandpass that varies in a predetermined manner as a function of said parameter.

8. The system of claim 5, further including:

equalizing means for compensating each of said first and second input signals with respect to the output of said midvalue selector to provide first and second equalization signals;

averaging means connected to said equalizing means for providing an average equalization signal representative of the average of said first and second equalization signals; and

means responsive to said suspected failure signal for selectively coupling said average equalization signal to said failure mode complementary filter, said average equalization signal being so coupled only when the difference between said redundant input signals is below said first predetermined threshold.

9. The system of claim 5 wherein said failure detection means includes:

rate monitoring and detecting means for monitoring the rate of deviation between the two redundant input signals applied to the first and second inputs of said midvalue selector and for generating a detected failure signal when said rate of deviation exceeds a predetermined threshold rate, said detected failure signal providing an indication that one of said redundant input signals is a failure; and

channel selection means for determining which one of said redundant input signals is a failure and, in response thereto, for isolating the output of said midvalue selector as an input to said normal mode complementary filter and for substituting therefore as an input to said normal mode complementary filter the one of said redundant input signals that is not a failure.

10. The system of claim 9, wherein said channel selection means includes:

input signal monitoring and detecting means for monitoring said first and second redundant input signals and for providing a failure confirmation signal when the difference between said redundant input signals exceeds a second predetermined threshold;

comparison means for comparing the difference between said first redundant input signal and a predetermined reference signal with the difference between said second redundant input signal and said predetermined reference signal to produce a difference signal;

channel-select signal generating means, connected to said comparison means, to said input signal monitoring and detecting means, and to said rate monitoring and detecting means, for generating a channel-select signal when the rate of deviation between said input signals exceeds said threshold rate, when the difference between said redundant input signals exceeds said second predetermined threshold, and when the difference signal produced by said comparison means exceeds a third predetermined threshold, said channel-select signal being indicative of the one of said redundant input signals that is not a failure; and

a channel-select switch connected to the output and first and second inputs of said midvalue selector and to the input of said normal mode complementary filter, said channel-select switch normally coupling the output of said midvalue selector to the input of said normal mode complementary filter, said channel-select switch being responsive to said channel-select signal to uncouple the output of said midvalue selector output from the input to said complementary filter and to selectively couple, as the input to said complementary filter, the one of said redundant input signals that is not a failure.

11. The system of claim 10, further including:

a fault monitoring complementary filter connected to receive said condition rate signal and the output of said midvalue selector, said filter producing a fault monitoring signal that is representative of said condition; and

wherein said fault monitoring signal is the predetermined reference signal used by said comparison means.

12. The system of claim 9, wherein:

said normal mode complementary filter includes first and second integrators, the output of said first integrator being provided as an input to said second integrator, the output of said second integrator comprising said failure mode complementary filter output signal; and

further including means responsive to said detected failure signal for selectively and momentarily coupling the outputs of the first and second integrators of said normal mode complementary filter to the first and second integrators, respectively, of said failure mode complementary filter.

13. The system of claim 12, wherein said condition rate signal is provided as an input to the second integrator of said failure mode complementary filter and wherein said filter includes means responsive to said suspected failure signal for disabling selected components of said filter such that only said second integrator is operable and said condition rate signal is the only input to said second integrator.