Home | Links | Contact Us | More About Intellectual Property | Bookmark
Search patents:
Home Telecommunications Sensor-device-for-a-missile

 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 ...


 Smart antenna channel simulator and test system
The essence of the present invention is a method and an apparatus to verify the integrity of a ...


 Sensor device for a missile

Details
Inventors: Strauss, Werner;
Assignee: Diehl GmbH & Co. (Nurnberg, DE)
Primary Examiner: Carone; Michael J.
Assistant Examiner: Montgomery; Christopher K.
Attorney, Agent or Firm: Scully, Scott, Murphy & Presser

Described is a sensor device (10) for a missile (16) having a matrix detector (12) and an electronic evaluation circuit connected thereto. A ray source (20) is stationarily arranged on the missile (16). Provided between the ray source (20) and the matrix detector (12) which is stationarily provided on the missile (16) is a gyro optical device (22) which is cardanically mounted in the missile (16). The sensor device may be employed to determine the roll position and roll rate of a missile (16).

DETAILED DESCRIPTION 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 expenditure is relatively low so that it is possible to provide a missile, in particular an autonomously guided missile, with simple means.
In a sensor device pursuant to the invention, the foregoing object is attained in that a ray source is arranged stationarily on the missile, and that a gyro-optical device is located between the ray source and the matrix detector, wherein the gyro-optical device is cardanically mounted in the missile.
The sensor device according to the invention has the advantages that it is of a relatively simple structure and is suitable for precisely ascertaining the respective positional angle and the respective rotational or roll rate of a missile by means of gyro-stabilised optical means and matrix detector which is fixed to the missile.
Autonomously guided missiles with imaging search head which usually involves an IR-search head involve the use of IR-matrix detectors which are usually cooled, in the search phase.
Such detectors have for example 128.
128 pixel elements.
By means of the sensor device according to the invention, it is possible to use the matrix detector which is preferably an IR-matrix detector in the flight phase of the projectile, which occurs in respect of time prior to the search phase, for determining the flight position and the roll speed, that is to say the speed of rotation, of the missile.
The sensor device according to the invention is suitable therefore not only for determining the flight position and rate of rotation in the flight phase which for example may involve a glide phase in order to achieve a maximum flight distance, but also for corresponding determination in the active target-search phase.
For that purpose, the invention provides for using an infra-red light source which is fixedly installed in the missile and which is preferably of dot configuration, and which is for example an LED infra-red diode



Related patents
  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 ...
  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 10-1, 10-2, . . . , 10-N and several radio receivers 20-1, 20-2, . . . ...

0.014

Archive: All patents - Links

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