RU95106258A - Radio altimeter - Google Patents
Radio altimeterInfo
- Publication number
- RU95106258A RU95106258A RU95106258/09A RU95106258A RU95106258A RU 95106258 A RU95106258 A RU 95106258A RU 95106258/09 A RU95106258/09 A RU 95106258/09A RU 95106258 A RU95106258 A RU 95106258A RU 95106258 A RU95106258 A RU 95106258A
- Authority
- RU
- Russia
- Prior art keywords
- output
- input
- pass filter
- low
- unit
- Prior art date
Links
Abstract
FIELD: radio engineering. SUBSTANCE: device has serial circuit of generator of linear frequency modulation pulses, generator of sound and heterodyne signals, amplifier, decoupling unit, and antenna. In addition device has serial circuit of first mixer, receiver, ranging unit, synchronization unit which generates temporary substitution. First output of latter unit is connected to input of generator of linear frequency modulation pulses; its second output is connected to second input of generator of sound and heterodyne signals. Second output of latter unit is connected to one input of first mixer, which second input is connected to output of decoupling unit. In addition device has second mixer, which output is connected to two channels first of which has third band-pass filter, first squarer and first low-pass filter. Second channel has fourth band-pass filter, second squarer and third low-pass filter. In addition device has third mixer which output is connected to two channels in parallel. First channel has fifth band-pass filter, third squarer, second low-pass filter. Second channel has sixth band-pass filter, fourth squarer, fourth low-pass filter. Output of first low-pass filter is connected to serial circuit of first adder, first subtraction unit and second adder. Second input of first adder output of second low-pass filter. Two channels are connected in parallel to output of second adder. First of these channels has first amplitude detector, fifth low-pass filter, which is connected to control input of third tuned heterodyne which output is connected to second input of second mixer and to input of first averaging counter, which output is connected to second input of digital adder, which first input is connected to third output of synchronization unit. Said second channel has second amplitude detector, sixth low-pass filter, which is connected to control input of fourth tuned heterodyne, which output is connected to second input of third mixer and to input of second averaging counter, which output is connected to third input of digital adder, which output serves as one of device outputs. It provides information about flight height of satellite. Output of second low-pass filter is connected to serial circuit of second subtraction unit, which second input is connected to output of first low-pass filter, third subtraction unit, which output is connected to control input of controlled amplifier, which input is connected to second input of second adder. Output of third low-pass filter is connected to serial circuit of third adder, which second input is connected to output of fourth low-pass filter, first attenuator, which output is connected to second input of first subtraction unit, and second attenuator, which output is connected to second input of third subtraction unit. Output of third subtraction unit serves as second device output, which provides analog information about height of roughness of ground surface. EFFECT: increased range of unambiguous measurement of flight height in real-time scale while keeping constant precision.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU95106258A RU2112250C1 (en) | 1995-04-20 | 1995-04-20 | Radio altimeter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU95106258A RU2112250C1 (en) | 1995-04-20 | 1995-04-20 | Radio altimeter |
Publications (2)
Publication Number | Publication Date |
---|---|
RU95106258A true RU95106258A (en) | 1997-01-20 |
RU2112250C1 RU2112250C1 (en) | 1998-05-27 |
Family
ID=20167005
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU95106258A RU2112250C1 (en) | 1995-04-20 | 1995-04-20 | Radio altimeter |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2112250C1 (en) |
-
1995
- 1995-04-20 RU RU95106258A patent/RU2112250C1/en active
Also Published As
Publication number | Publication date |
---|---|
RU2112250C1 (en) | 1998-05-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4521778A (en) | High-resolution, coherent pulse radar | |
Camps et al. | Optimization and performance analysis of interferometric GNSS-R altimeters: Application to the PARIS IoD mission | |
US3789409A (en) | Navigation system using satellites and passive ranging techniques | |
JP3785210B2 (en) | Parallel correlator for wide area positioning system | |
CA2025088A1 (en) | Device for locating a boring machine | |
Kanagaratnam et al. | Ultrawideband radar measurements of thickness of snow over sea ice | |
Rodriguez-Morales et al. | An improved UWB microwave radar for very long-range measurements of snow cover | |
Ecklund et al. | Crossed beam measurements of the diffuse radar aurora | |
Yao et al. | A novel low-power multifunctional ionospheric sounding system | |
EP0436302A2 (en) | Integrated altimeter and doppler velocity sensor arrangement | |
Haddrell et al. | Understanding the indoor GPS signal | |
RU95106258A (en) | Radio altimeter | |
RU2389040C1 (en) | Query method of measuring radial velocity and system for realising said method | |
RU2018864C1 (en) | Method of measuring distance in doppler speed vector meters for flying vehicles | |
Henry | Some developments in Loran | |
SU1366963A1 (en) | Panoramic reception device | |
RU2613865C2 (en) | Clock synchronisation method and device therefor | |
RU2204842C2 (en) | Method and device for measuring object-scattering polarization matrix | |
JPS59116073A (en) | Method and device for radio range finding | |
RU2327185C1 (en) | Nonlinear radar for eavesdropping devices | |
RU2305057C1 (en) | Determination of emergency object coordinates by elevation angle and time doppler method | |
RU2702190C1 (en) | Homodyne radar with antenna pattern scanning | |
RU2234717C1 (en) | Distance measuring apparatus | |
RU2602509C1 (en) | Method of generating a reference signal for combined processing of signals of standard and high accuracy of glonass system | |
SU982442A1 (en) | Ultrasonic meter of high pressure |