Home | Links | Contact Us | More About Intellectual Property | Bookmark
Search patents:
Home Telecommunications Horizon-sensor-for-satellites-using-superconductor-s-having-a-high-critical-temperature

 Radio test loop having common combiner cable connecting transmitters, spaced at n.lambda./2 therealong, with receivers, via frequency converter
OF A PREFERRED EMBODIMENT The radio unit shown in the figure comprises several radio transmitters 1...


 Method of equalizing a receive data block in a time-division multiple access communication system and receiver utilizing this method
An object of the invention is to remedy these drawbacks by proposing a method for equalizing a ...


 Method of intra-cell and inter-cell handover in a mobile communications system
According to the present invention there is provided a method for use in a cellular mobile ...


 Transceiver algorithms of antenna arrays
OF THE DISCLOSURE The invention is primarily intended for use in base stations for digital ...


 Simultaneous demodulation and decoding of a digitally modulated radio signal using known symbols
Referring to FIG. 1, a number of coded symbols to be conveyed to a receiver are marked "U" for ...


 Direct sequence spread spectrum receiver and antenna array for the simultaneous formation of a beam on a signal source and a null on an interfering jammer
OF THE PREFERRED EMBODIMENT A navigation satellite receiver system embodiment of the present ...


 Adaptive channel allocation in a frequency division multiplexed system
The present invention provides a method and system of adaptive channel allocation (ACA) in an ...


 Network utilizing modified preambles that support antenna diversity
These and other objects of the invention are achieved in a method for use in a communication ...


 Methods for channel estimation and signal detection of CDMA signals
The present invention is directed to a method for identifying the signature waveforms in CDMA ...


 Frequency-shifted feedback cavity used as a phased array antenna controller and carrier interference multiple access spread-spectrum transmitter
Therefore it is the principle object of the present invention to provide a novel and improved ...


 Horizon sensor for satellites using superconductor(s) having a high critical temperature

Details
Inventors: Sparvieri, Nicola; Graziani, Filippo;
Assignee: Selenia Industrie Elettroniche Associate S.p.A. (Rome, IT)
Primary Examiner: Hannaher; Constantine
Assistant Examiner:
Attorney, Agent or Firm: Cohen, Pontani, Lieberman & Pavane

A horizon sensor for spaced-based satellites consisting of a high critical temperature superconductor which changes temperature based upon its exposure to space-based radiation. The horizon sensor may be flexibly positioned along the outer surface of the space- based satellite. As the orientation in space of the satellite varies, certain portions of the satellite body will be alternately exposed to radiation while other portions of the satellite body will be shadowed from it. As the sensor is exposed to radiation due to the change in orientation of the satellite body, the temperature of the superconductor changes due to radiation absorption. This change in temperature causes the conductivity of the superconductor within the sensor to vary, and this causes a change in voltage within the sensor. This voltage may be appropriately processed via land based or satellite based control systems to accurately measure and/or change the orientation of the satellite in space.

DETAILED DESCRIPTION OF THE DRAWINGS In the drawings, wherein like reference characters denote similar elements throughout the several views: FIG.
1 illustrates a general block diagram of the horizon sensor of the instant invention; FIG.
2 shows the general circuit diagram of the horizon detector of the instant invention; FIG.
3 depicts the sensor mounted in a sealed cavity suitable for mounting on a satellite body; and FIG.
4 shows the sensor of FIG.
3 in position on a satellite.
DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS With initial reference to FIG.
1, there is shown a basic functional block diagram of the major components of the horizon sensor 10 of the instant invention.
An optical system 1 which is capable of passing space-based radiation is optically coupled to a radiation detecting element 2.
This radiation detecting element 2 is capable of sensing the presence of certain types of space-based radiation, changing temperature as a result of the quantity of exposure to such radiation, and emitting a voltage which conforms to said temperature change, said voltage being fed to a signal processor 3.
The optical system 1 allows for the selective passing and/or filtering of specific types and quantities of radiation, namely light and/or infrared radiation.
The signal processing element 3 may be a known signal processing means which can receive voltage signals from a sensor and pass along signals to be acted upon, for the purposes of monitoring or correcting the satellite's orientation in space.
FIG.
2 is an electrical schematic showing the detailed configuration of the radiation detector element 2.
FIG.
2 shows a high temperature superconductor, indicated as HTS, positioned in a commonly known resistor network.
As radiation which has been passed through optical system 1 impinges upon the high temperature superconductor the superconductor will change temperature.
Essentially, the high temperature superconductor reaches its lowest temperature in the absence of impinging radiation, and reaches its maximum temperature when the amount of radiation impinging upon it is at its maximum



Related patents
  Sensor device for a missile
The object of the present invention is to provide a sensor device of the kind set forth in the opening part of this specification, in which the level of structural ...
  Remote targeting system for guided missiles
What is claimed is: 1. In a remote target system for guided missiles, the combination comprising: (a) a radar located at a remote station for detecting and tracking a ...
  Detached and attached thermal spoilers for kinetic energy projectile fins
As in the prior art, a kinetic energy projectile intended to be launched toward a selected target has a projectile body and a plurality of main fins attached to the ...
  Image sensor and facsimile apparatus incorporating the same
Accordingly, it is an object of the present invention to eliminate the above-described problems in the related art and to provide an image sensor which facilitates the ...
  Image sensor and facsimile apparatus incorporating the same
Accordingly, it is an object of the present invention to eliminate the above-described problems of the prior art and to provide an image sensor which prevents the light ...
  Concentric broadband power combiner or divider
The present invention employs the principles of the above-mentioned linear multi-section network combiner but improves the basic design thereof by folding various ...
  Large scale low-loss combiner and divider
Referring now to FIG. 1A, one of the two parallel plates producing the radial waveguide of the device, namely 12, illustrated in FIG. 1B has been removed. The structure ...
  Steered-beam satellite communication system
The present invention provides a system for communicating via satellite between ground stations. The system comprises a set of ground stations spaced apart along an arc ...
  Compact signal isolating microwave splitters/combiners
OF EMBODIMENT Referring now to FIGS. 1-6, the reference numeral 20 designates a microwave assemblage of which the structure is functionally suitable for use as either a ...
  Testing transmitter-receiver apparatus for sector cell base station
It is an object of the present invention to provide a reliable testing transmitter-receiver apparatus for a sector cell base station wherein a testing antenna is ...

0.014

Archive: All patents - Links

Copyright (c)2006 Eipa-patents.org - All rights reserved