GB1207565A - Radio altimeters - Google Patents

Radio altimeters

Info

Publication number
GB1207565A
GB1207565A GB33046/68A GB3304668A GB1207565A GB 1207565 A GB1207565 A GB 1207565A GB 33046/68 A GB33046/68 A GB 33046/68A GB 3304668 A GB3304668 A GB 3304668A GB 1207565 A GB1207565 A GB 1207565A
Authority
GB
United Kingdom
Prior art keywords
height
counter
clock pulses
pulses
defining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB33046/68A
Inventor
Alexander Hammond Babb
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
STC PLC
Original Assignee
Standard Telephone and Cables PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Standard Telephone and Cables PLC filed Critical Standard Telephone and Cables PLC
Priority to GB33046/68A priority Critical patent/GB1207565A/en
Priority to CH1045269A priority patent/CH497709A/en
Priority to DE1935012A priority patent/DE1935012C3/en
Priority to FR6923502A priority patent/FR2012752A1/fr
Publication of GB1207565A publication Critical patent/GB1207565A/en
Priority to BE765118A priority patent/BE765118A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/02Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
    • G01S13/06Systems determining position data of a target
    • G01S13/08Systems for measuring distance only
    • G01S13/32Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated
    • G01S13/34Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal
    • G01S13/345Systems for measuring distance only using transmission of continuous waves, whether amplitude-, frequency-, or phase-modulated, or unmodulated using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal using triangular modulation
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating
    • G01S7/4052Means for monitoring or calibrating by simulation of echoes
    • G01S7/406Means for monitoring or calibrating by simulation of echoes using internally generated reference signals, e.g. via delay line, via RF or IF signal injection or via integrated reference reflector or transponder
    • G01S7/4065Means for monitoring or calibrating by simulation of echoes using internally generated reference signals, e.g. via delay line, via RF or IF signal injection or via integrated reference reflector or transponder involving a delay line

Abstract

1,207,565. Radio altimeter. STANDARD TELEPHONES & CABLES Ltd. 2 July, 1969 [11 July, 1968], No. 33046/68. Heading H4D. A radio altimeter, Fig. 2, comprises a transmitter 3 frequency modulated by a triangular waveform, Fig. la, and transmitting its output to: (a) a first receiver 10, both directly (path 4c) and via aerials 5, 9 and the ground return path, to produce therefrom a height/frequency dependant beat signal VF10, Fig. 1c; and (b) a second receiver 7, both directly (path 4b) and via a standard delay line 6, to produce therefrom a reference beat frequency signal VF7, Fig. 1b. A clock pulse generator 1 produces clock pulses, Fig. 1, and also pulses t o , defining the turn-over minimum of the modulation triangular waveform and t 1 , defining the start of the usable linear portion of said waveform. The wavelength of the reference beat frequency signal VF7 is determined in counter 8 by counting the number of clock pulses n rc in the first N R half cycles of said signal after t 1 , beginning at t 2 and ending at t 4 . Beat frequency signal VF10 is fed to counter 11 which is also fed with the clock pulses and pulses defining t 2 and t 4 . Counter 11 determines the number of half cycles No of VF10 from the commencement of the first crossover point after t 2 at time t 3 , to time t 5 of the first crossover point after t 4 , and also the number of clock pulses ng c occurring during period t 3 to t 5 . Signals representing the t 3 , t 4 , t 5 , N R and No are sent to computer 12, wherein the height is computed using the formula: N R and n rc should be equal to predetermined values whereby: Height = K . N G /n gc Values of N R and n rc are monitored at 15 and a detected error causes an alarm and/or shut down of the height information output. If N R and n rc can be assumed stable, outputs 8b and 8c of counter 8 can be omitted. If N G is large, then n gc #n rc , whereas (Fig. 2A, not shown): Height = K<SP>1</SP>N G .
GB33046/68A 1968-07-11 1968-07-11 Radio altimeters Expired GB1207565A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB33046/68A GB1207565A (en) 1968-07-11 1968-07-11 Radio altimeters
CH1045269A CH497709A (en) 1968-07-11 1969-07-09 Radio altimeter
DE1935012A DE1935012C3 (en) 1968-07-11 1969-07-10 FM-CW altimeter with triangular modulation and a reference receiver
FR6923502A FR2012752A1 (en) 1968-07-11 1969-07-10
BE765118A BE765118A (en) 1968-07-11 1971-04-01 RADIO ALTIMETER

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33046/68A GB1207565A (en) 1968-07-11 1968-07-11 Radio altimeters

Publications (1)

Publication Number Publication Date
GB1207565A true GB1207565A (en) 1970-10-07

Family

ID=10347812

Family Applications (1)

Application Number Title Priority Date Filing Date
GB33046/68A Expired GB1207565A (en) 1968-07-11 1968-07-11 Radio altimeters

Country Status (5)

Country Link
BE (1) BE765118A (en)
CH (1) CH497709A (en)
DE (1) DE1935012C3 (en)
FR (1) FR2012752A1 (en)
GB (1) GB1207565A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4107681A (en) * 1977-05-26 1978-08-15 Rockwell International Corporation Method and apparatus for automatically adjusting the resolution of a radio altimeter over its operating altitude range
FR2392396A1 (en) * 1977-05-26 1978-12-22 Rockwell International Corp METHOD AND APPARATUS FOR AUTOMATIC CALIBRATION OF A RADIO-ALTIMETER
CN102565768A (en) * 2011-12-29 2012-07-11 唐金元 Radio altitude signal simulator assembly based on surface acoustic wave delay lines
WO2014128687A1 (en) 2013-02-20 2014-08-28 Israel Aerospace Industries Ltd. System and method for testing frequency synthesizer
CN110873865A (en) * 2019-12-17 2020-03-10 陕西长岭电子科技有限责任公司 Vertical speed testing method of radio altimeter

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4468638A (en) * 1982-02-11 1984-08-28 The Bendix Corporation Linear sweep frequency modulator for FM/CW radio altimeter

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4107681A (en) * 1977-05-26 1978-08-15 Rockwell International Corporation Method and apparatus for automatically adjusting the resolution of a radio altimeter over its operating altitude range
FR2392396A1 (en) * 1977-05-26 1978-12-22 Rockwell International Corp METHOD AND APPARATUS FOR AUTOMATIC CALIBRATION OF A RADIO-ALTIMETER
CN102565768A (en) * 2011-12-29 2012-07-11 唐金元 Radio altitude signal simulator assembly based on surface acoustic wave delay lines
WO2014128687A1 (en) 2013-02-20 2014-08-28 Israel Aerospace Industries Ltd. System and method for testing frequency synthesizer
EP2959586A4 (en) * 2013-02-20 2016-10-12 Israel Aerospace Ind Ltd System and method for testing frequency synthesizer
US9921296B2 (en) 2013-02-20 2018-03-20 Israel Aerospace Industries Ltd. System and method for testing frequency synthesizer
CN110873865A (en) * 2019-12-17 2020-03-10 陕西长岭电子科技有限责任公司 Vertical speed testing method of radio altimeter
CN110873865B (en) * 2019-12-17 2023-03-21 陕西长岭电子科技有限责任公司 Vertical speed testing method of radio altimeter

Also Published As

Publication number Publication date
CH497709A (en) 1970-10-15
DE1935012C3 (en) 1975-07-17
FR2012752A1 (en) 1970-03-20
DE1935012A1 (en) 1970-02-26
BE765118A (en) 1971-10-01
DE1935012B2 (en) 1974-11-28

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees