Israel Aerospace Industries Ltd.

Liran Wiener

Vladimir Rojanski

Keren Boiman

A system and method for determination of a direction to an object emitting and/or reflecting electromagnetic radiation. The system includes a first pair of linearly polarized antennas configured for receiving a polarized signal of a first polarization type and a second pair of linearly polarized antennas configured for receiving another polarized signal of the polarization second type originated from the object. The system includes four receivers coupled to the linearly polarized antennas of the first and second pairs and a signal processing system coupled to the receivers. Each receiver associated with at least one pair of the antennas, includes a phase shifter to provide a required phase shift to the received polarized signals. The signal processing system combines the phase-shifted polarized signals with non-shifted signals which are originated from different pairs of the antennas, and to process these signals for generating at least one direction parameter of the object.

Radar system and method for determining direction to an object

A cover assembly is provided, for use with an instrument package having a common aperture. The cover assembly includes an inner cover member and an outer radome member. The inner cover member is substantially transparent to electromagnetic (EM) radiation of at least a first wavelength range. The radome member is configured for selectively and reversibly covering the inner cover member and transparent to EM radiation of at least a second wavelength range different from the first wavelength range. The second wavelength range includes a radio frequency wavelength range. The outer radome member is configured for being mounted in overlying relationship with respect to the common aperture of the instrument package. The radome member is configured for being initially in overlying relationship with respect to the inner cover member and for being selectively removed from the overlying relationship with respect to the inner cover member at least during flight conditions.

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Hod Hasharon, Israel

Liran Wiener