Other

Scaneva Ltd.

Apple Inc.

Technion Research & Development Foundation Limited

Enig Associates, Inc.

Elop Electrooptical Industries Ltd.

Elbit Systems Electro-optics Elop Ltd.

Mordekhai Velger

Yizhar Weiss

Raviv Erlich

Alexander Sromin

Sivan Natan-Knaz

Izhak Bucher

Yaron Zimmerman

Daniel Wormser

Atzmon Ofri

Boris Berg

Gergory Tocker

Yaacov Krispin

Boris Grinberg

A method of scanning a light beam is disclosed. The method comprises scanning the light beam along a first axis and scanning the light beam along a second axis, such that a functional dependence of the scanning along the first axis is substantially a step-wave, and a functional dependence of the scanning along the second axis is other than a step-wave.

Method and device for scanning light

A vibratory gyroscopic device to determine the rotation rate of an object and method of manufacturing thereof, the device including a plurality of supporting springs arranged in pairs to exhibit bilateral symmetry via each pair (i.e., mirror-image symmetry) relative to each other such that the asymmetries in the characteristics of the ring (e.g., resonant frequency, response to angular velocity), caused by asymmetries in the structure of the ring, are reduced.

Vibratory gyroscopic device for determining angular velocity

Geometric-waveform oscillator for processing light, the geometric waveform oscillator including a plurality of masses, at least one force producing element, and a plurality of elastic elements, each of the force producing elements being coupled with a respective one of the masses, at least one of the masses including a light processing module, each of the force producing elements applying a force to the masses, the elastic elements coupling the masses together, the elastic elements coupling the masses with a respective support, wherein the mass values of the masses, the force values of the forces, and the stiffness coefficients of the elastic elements, are selected such that the light processing module oscillates according to the geometric-waveform.

Oscillating mirror having a plurality of eigenmodes

An in-flight hose-and-drogue refueling system has the capability of steering the drogue using four thrusters which are energized by pressurized air. The system measures the drogue's 3-dimensional position relative to either the refueling aircraft or the probe on the receiver aircraft. A control system utilizes the measurements of the drogue's 3-dimensional position to activate the thrusters so as to either minimize the excursions of the drogue due to turbulence, thus enabling easier hook-up, or alternatively, to track the receiver's probe and automatically guide and contact the drogue to the probe.

Controllable hose-and-drogue in-flight refueling system

The invention provides a system for determining the spatial position of a moving object and for guiding its movement, which system comprises a triangular arrangement of three light sources attached to the moving object and facing guidance device, electrooptical sensing device comprising an area imaging device and an image processing computer located at a position facing the moving object, there being provided a guidance computer connected to the image processing computer, and radio-communication device for the exchange of signals from and to said moving object. As an alternative the three light sources can be provided at the ground station and the other components of the system being attached to the moving object, there being provided communication device between said station and object. The system is of special value for guiding manned and unmanned aircraft.

Aircraft automatic landing system

Growing community of inventors

Rehovot, Israel

Mordekhai Velger