Antenna stabilization error correction system for radar
First Claim
1. A radar system comprising:
- antenna controller and stabilization processor means connected to an aircraft attitude sensor;
antenna positioner means connected to said antenna controller and stabilization processor means;
antenna means connected to said antenna positioner means for transmitting signals, for receiving signals and for receiving ground clutter;
transmitter/receiver means connected to said antenna means;
signal processor means connected to said transmitter/receiver means, said antenna controller and stabilization processor means and an aircraft radio altimeter;
antenna stabilization error correction system connected to said signal processor means, said antenna controller and stabilization processor means and said aircraft radio altimeter means, wherein said antenna stabilization error correction system estimates pitch, roll and elevation errors and transmits corrected signals to said antenna controller and stabilization processor means;
said antenna stabilization error correction system includes compute incremental component means for computing .increment.Pe, .increment.R, .increment.Ee and .increment.T, wherein Pe is pitch error, Re is roll error, Ee is elevational error and T is time, compute slew rate limit means connected to said compute incremental component means, integrate means connected to said compute slew rate limit means for integrating .increment.Pe, .increment.Re, .increment.Ee and for providing Pe, Re, Ee, and magnitude limit means connected to said integrate means; and
said signal processor means extracting ground clutter signals from signals received from said transmitter/receiver means and sending said ground clutter signals to said antenna stabilization error correction system.
1 Assignment
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Accused Products
Abstract
A radar utilizes an antenna stabilization error correction system to automatically estimate and correct attitude sensor errors in pitch, roll and elevation. The radar system includes an antenna, an antenna positioner, a transmitter receiver, a signal processor, an antenna controller and stabilization processor and the antenna stabilization error correction system. As part of the normal signal processor sub function, ground clutter signals are extracted from the received signals. These signals are the primary input to the antenna stabilization error correction system. Other inputs are received from the signal processor, antenna controller and stabilization processor and an external aircraft radio altimeter. The antenna stabilization error correction system processes the signals and estimates pitch, roll and elevation errors which are passed back to the antenna controller and stabilization processor.
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Citations
8 Claims
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1. A radar system comprising:
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antenna controller and stabilization processor means connected to an aircraft attitude sensor; antenna positioner means connected to said antenna controller and stabilization processor means; antenna means connected to said antenna positioner means for transmitting signals, for receiving signals and for receiving ground clutter; transmitter/receiver means connected to said antenna means; signal processor means connected to said transmitter/receiver means, said antenna controller and stabilization processor means and an aircraft radio altimeter; antenna stabilization error correction system connected to said signal processor means, said antenna controller and stabilization processor means and said aircraft radio altimeter means, wherein said antenna stabilization error correction system estimates pitch, roll and elevation errors and transmits corrected signals to said antenna controller and stabilization processor means; said antenna stabilization error correction system includes compute incremental component means for computing .increment.Pe, .increment.R, .increment.Ee and .increment.T, wherein Pe is pitch error, Re is roll error, Ee is elevational error and T is time, compute slew rate limit means connected to said compute incremental component means, integrate means connected to said compute slew rate limit means for integrating .increment.Pe, .increment.Re, .increment.Ee and for providing Pe, Re, Ee, and magnitude limit means connected to said integrate means; and said signal processor means extracting ground clutter signals from signals received from said transmitter/receiver means and sending said ground clutter signals to said antenna stabilization error correction system. - View Dependent Claims (2, 3, 4, 5)
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6. A radar system comprising:
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antenna controller and stabilization processor means connected to an aircraft attitude sensor; antenna positioner means connected to said antenna controller and stabilization processor means; antenna means connected to said antenna positioner means for transmitting signals, for receiving signals and for receiving ground clutter; transmitter/receiver means connected to said antenna means; signal processor means connected to said transmitter/receiver means, said antenna controller and stabilization processor means and an aircraft radio altimeter; and
,antenna stabilization error correction system connected to said signal processor means, said antenna controller and stabilization processor means and said aircraft radio altimeter means, wherein said signal processor means extracts ground clutter signals from signals received from said transmitter/receiver means and sends said ground clutter signals to said antenna stabilization error correction system and wherein said antenna stabilization error correction system estimates stabilization error, Θ
e, wherein ##EQU3## where N is number of qualified clutter patches;
where Z is aircraft altitude;where Ri is slant range to clutter patch i; where K is dependent upon said antenna means specific to said radar system application; where .increment.dBi is estimated clutter power changes in a particular clutter patch i; where .increment.Θ
ct is a small perturbation in antenna tilt; and
,where Θ
ct is average commanded tilt angle about which tilt angle is perturbed. - View Dependent Claims (7)
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8. A radar system comprising:
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antenna controller and stabilization processor means connected to an aircraft attitude sensor; antenna positioner means connected to said antenna controller and stabilization processor means; antenna means connected to said antenna positioner means for transmitting signals, for receiving signals and for receiving ground clutter; transmitter/receiver means connected to said antenna means; signal processor means connected to said transmitter/receiver means, said antenna controller and stabilization processor means and an aircraft radio altimeter; antenna stabilization error correction system connected to said signal processor means, said antenna controller and stabilization processor means and said aircraft radio altimeter means, wherein said antenna stabilization error correction system estimates pitch, roll and elevation errors and transmits corrected signals to said antenna controller and stabilization processor means; said antenna stabilization error system estimates stabilization error, Θ
e, wherein ##EQU4## Where N is number of qualified clutter patches;
where Z is aircraft altitude;where Ri is slant range to clutter patch i; where K is dependent upon said antenna means specific to said radar system application; where .increment.dBi is estimated clutter power changes in a particular clutter patch i; where .increment.Θ
ct is a small perturbation in antenna tilt; and
,where Θ
ct is average commanded tilt angle about which tilt angle is perturbed.
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Specification