| Class / Patent application number | Description | Number of patent applications / Date published |
|---|
| 244300190 | Radio wave | 7 |
| 20100282894 | Antenna pointing bias estimation using radar imaging - A system for estimating an antenna boresight direction. The novel system includes a first circuit for receiving a Doppler measurement and a line-of-sight direction measurement corresponding with the Doppler measurement, and a processor adapted to search for an estimated boresight direction that minimizes a Doppler error between the Doppler measurement and a calculated Doppler calculated from the estimated boresight direction and the line-of-sight direction measurement. The line-of-sight direction measurement is measured relative to the true antenna boresight, and the calculated Doppler is the Doppler calculated for a direction found by applying the line-of-sight direction measurement to the estimated boresight direction. In a preferred embodiment, the first circuit receives a Doppler measurement and a line-of-sight direction measurement from each of a plurality of pixels, and the processor searches for an estimated boresight direction that minimizes a sum of squares of Doppler errors for each of the pixels. | 11-11-2010 |
| 20110240792 | TRANSMISSION OF INFORMATION TO A SYSTEM UTILIZING A GPS DEVICE - A system for transmitting non-GPS information for reception by a global positioning system (GPS) receiver, the system including a processor, a memory coupled to the processor and including computer-readable instructions configured to, when executed by the processor, cause the processor to receive the non-GPS information, determine an available pseudo-random noise (PRN) code, spread the non-GPS information using the available PRN code to provide a spread signal, modulate a GPS carrier frequency using the spread signal to produce a GPS compatible signal, and a terrestrial transmitter configured to transmit the GPS compatible signal. | 10-06-2011 |
| 20120181374 | MONOPULSE SPIRAL MODE ANTENNA COMBINING - A technique employing one or more conformal, spiral antenna for use in a vehicle such as a missile. The technique includes both an apparatus and a method. The apparatus includes a radome or missile body and a conformal, spiral antenna mounted in the radome or missile body. The method is one for use in operating a missile, comprising transmitting and receiving signals through a plurality of conformal, spiral antennae mounted in a radome or missile body. This may include in some variants transmitting and receiving signals through a plurality of conformal, spiral antennae mounted in a radome or missile body; and guiding the missile from information obtained from signals receive through the antennae. | 07-19-2012 |
| 20120199690 | SYSTEM AND METHOD FOR ROLL ANGLE INDICATION AND MEASUREMENT IN FLYING OBJECTS - A method for onboard determination of a roll angle of a projectile. The method including: transmitting a polarized RF signal from a reference source, with a predetermined polarization plane; receiving the signal at a pair of polarized RF sensor cavities positioned symmetrical on the projectile with respect to the predetermined polarization plane; receiving the signal at a third polarized RF sensor cavity positioned such that it receives a maximum signal at zero roll angle positioning; differentiating between up or down positioning of the desired roll angle position based on an output from a fourth sensor on the projectile; analyzing an output of the pair of polarized RF sensor cavities and the third RF sensor cavity resulting from the received signal and an output of the fourth sensor; generating a curve based on the output of the pair of polarized RF sensor cavities and the third RF sensor cavity indicating a relationship between roll angle and the third sensor output; and determining a roll angle positioning of the projectile based on the curve. | 08-09-2012 |
| 20130001354 | GPS independent guidance sensor system for gun-launched projectiles - A sensor system uses ground emitters to illuminate a projectile in flight with a polarized RF beam. By monitoring the polarization modulation of RF signals received from antenna elements mounted on the projectile, both angular orientation and angular rate signals can be derived and used in the inertial solution in place of the gyroscope. Depending on the spacing and positional accuracies of the RF ground emitters, position information of the projectile may also be derived, which eliminates the need for accelerometers. When RF signals of ground emitter/s are blocked from the guided projectile, the sensor deploys another plurality of RF antennas mounted on the projectile nose to determine position and velocity vectors and orientation of incoming targets. | 01-03-2013 |
| 20160003579 | A MISSILE SEEKER AND GUIDANCE METHOD - In a method of guiding a missile in flight to a target (FIG. | 01-07-2016 |
| 20160131456 | IMPROVEMENTS IN AND RELATING TO MISSILE SEEKERS - A sensor for a missile seeker includes a primary, concave, reflector that is reflective to RF waves and to another kind of waves, but that includes a transmissive region, through which RF waves can pass. A secondary, convex, reflector is reflective to RF waves but transmissive, and not reflective, to the other kind of waves, and is arranged facing the primary reflector to further reflect RF waves reflected by the primary reflector through the transmissive region of the primary reflector. An RF detector is arranged on the opposite side of the primary reflector from the secondary reflector and arranged to detect the RF waves reflected by the secondary reflector through the transmissive region of the primary reflector. A second detector, for detecting the other kind of waves, is arranged on the opposite side of the secondary reflector from the primary reflector and is arranged to detect the other kind of waves after they are reflected by the primary reflector and transmitted through the secondary reflector. | 05-12-2016 |
