Barometric altimeter

• US 4,253,335 A
• Filed: 05/18/1979
• Issued: 03/03/1981
• Est. Priority Date: 12/28/1978
• Status: Expired due to Term

• Current Assignee: Naonobu Shimomura
• Original Assignee: Naonobu Shimomura
• Inventors: Shimomura, Naonobu
• Primary Examiner(s): WOODIEL, DONALD
• Application Number:
  US06/040,409
• Time in Patent Office: 655 Days
• Field of Search: 73/384, 73/386, 73/387
• US Class Current: 73/384
• CPC Class Codes: G01C 5/06 by using barometric means

Abstract

The altitude of an aircraft is determined by measuring the output of a pressure transducer on the aircraft because the altitude is defined by the atmospheric pressure at that point. In this altitude measurement, the relationship between the altitude and the atmospheric pressure is nonlinear, and most pressure transducers exhibit some nonlinearity. High accuracy altitude measurement, correcting those nonlinearities, have been disclosed in the prior art utilizing a quasi-exponential function generator (QEFG). A quasi-exponential function is an exponential function with a time constant which varies with time. However, the characteristics of the pressure transducer and QEFG are affected by temperature, and there have been no appropriate means other than the use of a thermostat to maintain the accuracy of measurement when the temperature varies. This invention compensates for the temperature variant characteristics of the pressure transducer and the QEFG by changing the constants of the circuit elements of the QEFG and of the output stage coupled to the pressure transducer according to the output of a temperature sensor incorporated in the altimeter. Even the change of nonlinearity, or the change of curvature of the characteristic curve of the pressure transducer is compensated for almost perfectly by this invention.

Claims

1. Pressure altitude measuring apparatus comprising:

a pressure sensor which produces a first electrical signal representing the atomospheric pressure at the altitude to be measured and containing a pressure transducer that produces an electrical output in response to the pressure applied thereon and an output stage with a resistor circuit to compensate for the offset value of the electrical output of said pressure transducer and a resistor circuit to adjust the magnitude of said first electrical signal,

means to produce at least one kind of second electrical signals approximately equal respectively to the electrical signals which would be produced by said pressure sensor when the atmosheric pressure of at least one kind of altitude measuring reference altitudes is applied thereon,

a quasi-exponential function generator comprising a capacitor circuit with two terminals, a discharge resistor circuit with two terminals and a controller, said two terminal discharge resistor circuit comprising at least one resistor and at least one switch for said function generation and controlled to provide an effective resistance which decreases with time by means of controlling said at least one switch for said function generation by said controller, and each of said two terminals of said discharge resistor circuit is connected to each of said two terminals of said capacitor circuit,

means to generate a third electrical signal by means of charging said capacitor circuit of said quasi-exponential function generator with an electrical voltage determined in relation to the magnitude of the signal of the largest one of said at least one kind of second electrical signals, and discharging through said discharge resistor circuit for a predetermined discharging period in which said controller controls to decrease the effective resistance of said discharge resistor circuit,

counting means to count electrical pulses of a predetermined frequency,

means to control said counting means to count said electrical pulses only during the time interval in which the magnitude of said third electrical signal is approximately not more than the magnitude of one of said second electrical signals and not less than the magnitude of said first electrical signal,

a temperature sensing device including temperature sensor, said device exhibiting plural electrical states according to the temperature of said pressure sensor and said quasi-exponential function generator,

temperature compensation means comprising at least one of the following four means;

(1) means to change the electrical capacity of said capacitor circuit of said quasi-exponential function generator including controlling switches for temperature compensation incorporated in said capacitor circuit,

(2) means to change the resistance of said discharge resistor circuit of said quasi-exponential function generator including controlling switches for temperature compensation incorporated in said discharge resistor circuit,

(3) means to change the resistance of said resistor circuit to compensate for the offset value in said output stage of said pressure sensor including controlling switches for temperature compensation incorporated in said resistor circuit to compensate for the offset value,

(4) means to change the resistance of said resistor circuit to adjust the magnitude of said first electrical signal in said output stage of said pressure sensor including controlling switches for temperature compensation incorporated in said resistor circuit to adjust the magnitude of said first electrical signal, according to said electrical states of said temperature sensing device,

wherein a temperature compensated pressure altitude is obtained in said counting means.

3. Apparatus as claimed in claim 1, wherein said temperature sensor produces an electrical signal in response to the temperature of said pressure sensor and said quasi-exponential function generator, said electrical signal produced by said temperature sensor being converted to a first digital signal, and one of said plural electrical states exhibited by said temperature sensing device is represented by a second digital signal converted from said first digital signal by means for referencing a conversion table stored in a memory and prescribed by the temperature characteristics of said temperature sensor, said pressure sensor and said quasi-exponential function generator, and said control of said controlling switches for temperature compensation effected in response to corresponding bits of said second digital signal.

5. Apparatus as claimed in claim 1, wherein said temperature sensor produces an electrical signal in response to the temperature of said pressure sensor and said quasi-exponential function generator and one of said plural electrical states exhibited by said temperature sensing device is represented by a set of electrical signals appearing at a plurality of output terminals of a level detector, said level detector produces electrical signals at its output terminals in succession in response to the magnitude of said electrical signal produced by said temperature sensor, and said control of said controlling switches for temperature compensation effected in response to corresponding electrical signals appearing at said plurality of output terminals of said level detector.

7. Apparatus as claimed in claims 1, 3 or 5, wherein said discharging period is divided into a plurality of time intervals and said capacitor circuit of said quasi-exponential function generator has terminals 1 and 2, and said discharge resistor circuit comprises n resistors r_i (where i=0, 1, 2, . . . , n-1 and n is an integer), each resistor r_i has terminals 1_i and 2_i, and n switches Sd_i for said function generation, each switch Sd_i has terminals 3_i and 4_i, and said terminal 1_i of said resistor r_i is connected to said terminal 1 of said capacitor circuit, and said terminal 2_i of said resistor r_i is connected to said terminal 3_i of said switch Sd_i respectively, and said terminal 4_i of said switch Sd_i is connected to said terminal 2 of said capacitor circuit, and said switch Sd_i is controlled by said controller to be turned on only for the i th time interval of said discharging period, and wherein at least one of said resistors r_i '"'"'s is an adjustable resistor, whereby the altitude obtained in said counting means may be adjusted to correspond with the altitude measured by another altimeter.

8. Apparatus as claimed in claim 7, wherein there is further included means to easily adjust said electrical voltage for charging said capacitor circuit of said quasi-exponential function generator to a value slightly different from the magnitude of the largest one of said second electrical signals, and to control counting of said counting means to start at the instant of the start of the discharge of said capacitor circuit of said quasi-exponential function generator and to stop at the instant of said third electrical signal becomes equal to said first electrical signal whereby the value of the altitude obtained in said counting means corresponds with the altitude measured by another altimeter in a predetermined lower range of altitudes.

9. Apparatus as claimed in claim 8, wherein said one kind of altitude measuring reference altitude is set to -1050 ft, and said counting means comprises first counter of modulus ten, and second counter of modulus five and preset with two, and third counter of binary mode, and said first counter and said second counter count electrical pulses each of which represents one hundred feet increment of altitude, and said third counter counts overflow pulses from said second counter, and there are further included means to convert the binary number counted in said third counter to gray code and send out as the higher order bits of an altitude reporting code, and also to convert the number counted in said first counter to a three bit code according to a prescribed conversion table and send out as the lower order three bits of an altitude reporting code.

10. Apparatus as claimed in claim 7, wherein said one kind of altitude measuring reference altitude is set to -1050 ft, and said counting means comprises first counter of modulus ten, and second counter of modulus five and preset with two, and third counter of binary mode, and said first counter and said second counter count electrical pulses each of which represents one hundred feet increment of altitude, and said third counter counts overflow pulses from said second counter, and there are further included means to convert the binary number counted in said third counter to gray code and send out as the higher order bits of an altitude reporting code, and also to convert the number counted in said first counter to a three bit code according to a prescribed conversion table and send out as the lower order three bits of an altitude reporting code.

11. Apparatus as claimed in claims 1, 3, or 5, wherein said discharging period is divided into a plurality of time intervals and said capacitor circuit of said quasi-exponential function generator has two terminals, and said discharge resistor circuit which has two terminals comprises the serial connection of first resistor circuit formed by a resistor r and second resistor circuit containing n resistors r_i (where i=0, 1, 2, . . . , n-1 and n is an integer), each resistor r_i has terminals 1_i and 2_i, and n switches Sd_i for said function generation, each of which has terminals 3_i and 4_i, and said terminals 1_i '"'"'s of said resistor r_i '"'"'s are all connected together to form one terminal of said second resistor circuit, and said terminal 2_i of said resistor r_i is connected to said terminal 3_i of said switch Sd_i respectively, and said terminals 4_i '"'"'s of said switches Sd_i '"'"'s are all connected together to form the other terminal of said second resistor circuit, and said two terminals of said discharge resistor circuit are connected respectively to said two terminals of said capacitor circuit, and said switch Sd_i is controlled by said controller to be turned on only for the i th time interval of said discharging period, and wherein at least one of said resistors r_i '"'"'s is an adjustable resistor, whereby the altitude obtained in said counting means may be adjusted to correspond with the altitude measured by another altimeter.

12. Apparatus as claimed in claim 11, wherein said one kind of altitude measuring reference altitude is set to -1050 ft, and said counting means comprises first counter of modulus ten, and second counter of modulus five and preset with two, and third counter of binary mode, and said first counter and said second counter count electrical pulses each of which represents one hundred feet increment of altitude, and said third counter counts overflow pulses from said second counter, and there are further included means to convert the binary number counted in said third counter to gray code and send out as the higher order bits of an altitude reporting code, and also to convert the number counted in said first counter to a three bit code according to a prescribed conversion table and send out as the lower order three bits of an altitude reporting code.

13. Apparatus as claimed in claim 11, wherein there is further included means to easily adjust said electrical voltage for charging said capacitor circuit of said quasi-exponential function generator to a value slightly different from the magnitude of the largest one of said second electrical signals, and to control counting of said counting means to start at the instant of the start of the discharge of said capacitor circuit of said quasi-exponential function generator and to stop at the instant of said third electrical signal becomes equal to said first electrical signal whereby the value of the altitude obtained in said counting means corresponds with the altitude measured by another altimeter in a predetermined lower range of altitudes.

14. Apparatus as claimed in claim 13, wherein said one kind of altitude measuring reference altitude is set to -1050 ft, and said counting means comprises first counter of modulus ten, and second counter of modulus five and preset with two, and third counter of binary mode, and said first counter and said second counter count electrical pulses each of which represents one hundred feet increment of altitude, and said third counter counts overflow pulses from said second counter, and there are further included means to convert the binary number counted in said third counter to gray code and send out as the higher order bits of an altitude reporting code, and also to convert the number counted in said first counter to a three bit code according to a prescribed conversion table and send out as the lower order three bits of an altitude reporting code.

15. Apparatus as claimed in claims 1, 2, 3, 4, 5 or 6, wherein said means to produce one kind of second electrical signal comprises a first resistor, a potentiometer which has two fixed terminals and one sliding contact terminal, a second resistor, a mechanical display device which indicates barometric setting, and a rotating knob which drives said sliding contact of said potentiometer and said display device through a mechanism by which the movements of both said sliding contact of said potentiometer and said display device are kept in linear relation with the angle of rotation of said knob, and one terminal of said first resistor is connected to one terminal of power supply, the other terminal of said first resistor is connected to one fixed terminal of said potentiometer, the other fixed terminal of said potentiometer is connected to one terminal of said second resistor, and the other terminal of said second resistor is connected to the other terminal of power supply, and said one kind of second electrical signal is obtained at the sliding contact terminal of said potentiometer when said knob is operated to indicated the value of the barometric setting in said mechanical display device.

16. Apparatus as claimed in claim 15, wherein there is further included display means to indicate said altitude obtained in said counting means by a rotating drum display, said display means comprises a rotating drum display consisting of first, second, third and fourth rotating drums each equipped with an encoder, and a servomotor and a servo-circuit, and said servomotor drives said first rotating drum and is driven by the output of said servo-circuit, and periphery of said first rotating drum is scaled with indications of 00 ft through 90 ft with 10 ft steps, periphery of said second rotating drum is scaled with indications of 0 through 9 with 100 ft steps, periphery of said third rotating drum is scaled with indications 0 through 9 with 1000 ft steps, periphery of said fourth rotating drum is scaled with indications of appropriate numbers among 0 through 9 as necessary to indicate the measured altitude with 10000 ft steps, and said first rotating drum is mechanically linked with said second rotating drum so that for the rotation of 90 to 00 of said first rotating drum, the indication of said second rotating drum is incremented, and for the rotation of 00 to 90 of said first rotating drum, the indication of said second rotating drum is decremented, and said second rotating drum is mechanically linked with said third rotating drum so that for the rotation of said second rotating drum from 9 to 0, the indication of said third rotating drum is incremented, and for the rotation of said second rotating drum from 0 to 9, the indication of said third rotating drum is decremented, and said third rotating drum is mechanically linked with said fourth rotating drum so that for the rotation from 9 to 0 of said third rotating drum, the indication of said fourth rotating drum is incremented, and for the rotation from 0 to 9 of said third rotating drum, the indication of said fourth rotating drum is decremented, and said encoder for said first rotating drum generates gray code 0 through 2ⁿ -1 (where n is an integer), and each of said encoder for said second and third rotating drums generates a code which changes only one bit for the increment of indications of 0, 1, 2, . . . , 9, 0, and said encoder for said fourth rotating drum generates a code which changes only one bit for the increment of indications necessary to indicate measured altitude, and the difference of the output value of said encoders of said rotating drum display and said altitude obtained in said counting means is converted to analog value and supplied to the input of said servo-circuit as an error signal whereby said servomotor drives said rotating drum display to track said altitude obtained in said counting means.

17. Apparatus as claimed in claim 16, wherein there are further included means to indicate the selected altitude by a mechanical display with an encoder where said mechanical display to indicate the selected altitude is driven manually and said encoder generates a digital signal representing the indication of said mechanical display to indicate the selected altitude, means to calculate the difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means, means to compare said difference value with at least one pair of predetermined numerical values stored in a memory, and means to produce at least one alert signal when said difference value exists between said at least one pair of predetermined numerical values.

18. Apparatus as claimed in claim 17, wherein there is further included means to send out said difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means to an autopilot as one of the control signals therefor.

19. Apparatus as claimed in claim 15, wherein there are further included means to indicate the selected altitude by a mechanical display with an encoder where said mechanical display to indicate the selected altitude is driven manually and said encoder generates a digital signal representing the indication of said mechanical display to indicate the selected altitude, means to calculate the difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means, means to compare said difference value with at least one pair of predetermined numerical values stored in a memory, and means to produce at least one alert signal when said difference value exists between said at least one pair of predetermined numerical values.

20. Apparatus as claimed in claim 19, wherein there is further included means to send out said difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means to an autopilot as one of the control signals therefor.

21. Apparatus as claimed in claims 1, 2, 3, 4, 5 or 6, wherein said one kind of altitude measuring reference altitude is set to -1050 ft, and said counting means comprises first counter of modulus ten, and second counter of modulus five and preset with two, and third counter of binary mode, and said first counter and said second counter count electrical pulses each of which represents one hundred feet increment of altitude, and said third counter counts overflow pulses from said second counter, and there are further included means to convert the binary number counted in said third counter to gray code and send out as the higher order bits of an altitude reporting code, and also to convert the number counted in said first counter to a three bit code according to a prescribed conversion table and send out as the lower order three bits of an altitude reporting code.

22. Apparatus as claimed in claims 1, 2, 3, 4, 5 or 6, wherein there is further included display means to indicate said altitude obtained in said counting means by a rotating drum display, said display means comprises a rotating drum display consisting of first, second, third and fourth rotating drums each equipped with an encoder, and a servomotor and a servo-circuit, and said servomotor drives said first rotating drum and is driven by the output of said servo-circuit, and periphery of said first rotating drum is scaled with indications of 00 ft through 90 ft with 10 ft steps, periphery of said second rotating drum is scaled with indications of 0 through 9 with 100 ft steps, periphery of said third rotating drum is scaled with indications 0 through 9 with 1000 ft steps, periphery of said fourth rotating drum is scaled with indications of appropriate numbers among 0 through 9 as necessary to indicate the measured altitude with 10000 ft steps, and said first rotating drum is mechanically linked with said second rotating drum so that for the rotation of 90 to 00 of said first rotating drum, the indication of said second rotating drum is incremented, and for the rotation of 00 to 90 of said first rotating drum, the indication of said second rotating drum is decremented, and said second rotating drum is mechanically linked with said third rotating drum so that for the rotation of said second rotating drum from 9 to 0, the indication of said third rotating drum is incremented, and for the rotation of said second rotating drum from 0 to 9, the indication of said third rotating drum is decremented, and said third rotating drum is mechanically linked with said fourth rotating drum so that for the rotation from 9 to 0 of said third rotating drum, the indication of said fourth rotating drum is incremented, and for the rotation from 0 to 9 of said third rotating drum, the indication of said fourth rotating drum is decremented, and said encoder for said first rotating drum generates gray code 0 through 2ⁿ -1 (where n is an integer), and each of said encoder for said second and third rotating drums generates a code which changes only one bit for the increment of indications of 0, 1, 2, . . . , 9, 0, and said encoder for said fourth rotating drum generates a code which changes only one bit for the increment of indications necessary to indicate measured altitude, and the difference of the output value of said encoders of said rotating drum display and said altitude obtained in said counting means is converted to analog value and supplied to the input of said servo-circuit as an error signal whereby said servomotor drives said rotating drum display to track said altitude obtained in said counting means.

23. Apparatus as claimed in claim 22, wherein there are further included means to indicate the selected altitude by a mechanical display with an encoder where said mechanical display to indicate the selected altitude is driven manually and said encoder generates a digital signal representing the indication of said mechanical display to indicate the selected altitude, means to calculate the difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means, means to compare said difference value with at least one pair of predetermined numerical values stored in a memory, and means to produce at least one alert signal when said difference value exists between said at least one pair of predetermined numerical values.

24. Apparatus as claimed in claim 23, wherein there is further included means to send out said difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means to an autopilot as one of the control signals therefor.

25. Apparatus as claimed in claims 1, 2, 3, 4, 5 or 6, wherein there are further included means to indicate the selected altitude by a mechanical display with an encoder where said mechanical display to indicate the selected altitude is driven manually and said encoder generates a digital signal representing the indication of said mechanical display to indicate the selected altitude, means to calculate the difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means, means to compare said difference value with at least one pair of predetermined numerical values stored in a memory, and means to produce at least one alter signal when said difference value exists between said at least one pair of predetermined numerical values.

26. Apparatus as claimed in claim 25, wherein there is further included means to send out said difference value of said digital signal generated by said encoder of said mechanical display to indicate the selected altitude and said altitude obtained in said counting means to an autopilot as one of the control signals therefor.

2. Pressure altitude measuring apparatus comprising:

a pressure sensor which produces a first electrical signal representing the atmospheric pressure at the altitude to be measured and containing a pressure transducer that produces an electrical output in response to the pressure applied thereon and an output stage with a resistor circuit to compensate for the offset value of the electrical output of said pressure transducer and a resistor circuit to adjust the magnitude of said first electrical signal,

means to produce at least one kind of second electrical signals approximately equal respectively to the electrical signals which would be produced by said pressure sensor when the atmospheric pressure of at least one kind of altitude measuring reference altitudes is applied thereon,

a quasi-exponential function generator comprising a capacitor circuit with two terminals and a discharge resistor circuit with two terminals and a controller, said capacitor circuit comprising a main capacitor which forms the main part of the capacity of said capacitor circuit and plural number of sectional capacitors which are connected in parallel to said main capacitor respectively by plural number of switches for said function generation, and said controller controls said plural number of switches for said function generation, and said controller controls said plural number of switches for said function generation to disconnect said plural number of sectional capacitors in a sequence of time from said main capacitor, and each of said two terminals of said discharge resistor circuit is connected to each of said two terminals of said capacitor circuit,

means to generate a third electrical signal by means of charging said capacitor circuit of said quasi-exponential function generator with an electrical voltage determined in relation to the signal of the largest one of said at least one kind of second electrical signals, and discharging through said discharge resistor circuit for a predetermined discharging period which said controller controls to disconnect said sectional capacitors from said main capacitor in a sequence of time,

counting means to count electrical pulses of a predetermined frequency,

means to control said counting means to count said electrical pulses only during the time interval in which the magnitude of said third electrical signal is approximately not more than the magnitude of one of said second electrical signals and not less than the magnitude of said first electrical signal,

a temperature sensing device including temperature sensor, said device exhibiting plural electrical states according to the temperature of said pressure sensor and said quasi-exponential function generator,

temperature compensation means comprising at least one of the following four means;

(1) means to change the electrical capacity of said capacitor circuit of said quasi-exponential function generator including controlling switches for temperature compensation incorporated in said capacitor circuit,

(2) means to change the temperature of said discharge resistor circuit of said quasi-exponential function generator including controlling switches for temperature compensation incorporated in said discharge resistor circuit,

(3) means to change the resistance of said resistor circuit to compensate for the offset value in said output stage of said pressure sensor including controlling switches for temperature compensation incorporated in said resistor circuit to compensate for the offset value,

(4) means to change the resistance of said resistor circuit to adjust the magnitude of said first electrical signal in said output stage of said pressure sensor including controlling switches for temperature compensation incorporated in said resistor circuit to adjust the magnitude of said first electrical signal, according to said electrical states of said temperature sensing device,

wherein a temperature compensated pressure altitude is obtained in said counting means.

4. Apparatus as claimed in claim 2, wherein said temperature sensor produces an electrical signal in response to the temperature of said pressure sensor and said quasi-exponential function generator, said electrical signal produced by said temperature sensor being converted to a first digital signal, and one of said plural electrical states exhibited by said temperature sensing device is represented by a second digital signal converted from said first digital signal by means for referencing a conversion table stored in a memory and prescribed by the temperature characteristics of said temperature sensor, said pressure sensor and said quasi-exponential function generator, and said control of said controlling switches for temperature compensation effected in response to corresponding bits of said second digital signal.

6. Apparatus as claimed in claim 2, wherein said temperature sensor produces an electrical signal in response to the temperature of said pressure sensor and said quasi-exponential function generator and one of said plural electrical states exhibited by said temperature sensing device is represented by a set of electrical signals appearing at a plurality of output terminals of a level detector, said level detector produces electrical signals at its output terminals in succession in response to the magnitude of said electrical signal produced by said temperature sensor, and said control of said controlling switches for temperature compensation effected in response to corresponding electrical signals appearing at said plurality of output terminals of said level detector.