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A projectile for launching by a cannon or by a launcher is obtained by an expedient combination of features. An optical seeker has a gyro mounted on an air bearing and an optical detector. a Cassegrain system is arranged on the gyro as imaging optical system and scans a field of view with a gyrating

A projectile for launching by a cannon or by a launcher is obtained by an expedient combination of features. An optical seeker has a gyro mounted on an air bearing and an optical detector. a Cassegrain system is arranged on the gyro as imaging optical system and scans a field of view with a gyrating scanning motion. At its tip, the projectile is closed by an optically transparent wedge, which is limited by planar surfaces. The optically transparent wedge carries a central spike. The projectile has tail stabilizing fins and steering by wings arranged near the center of gravity of the projectile. The wings are controlled by signals from the detector through signal processing means and an actuator system. The projectile is shaped make a continuous roll movement due to aerodynamic forces.

대표청구항 ▼

A projectile with steering means for steering the projectile onto a target during the end phase of its trajectory, characterized by the combination of the following features: (a) An optical seeker (12) comprises a gyro (18) with a gyro rotor supported, in operation, by compressed air supplied to a g

A projectile with steering means for steering the projectile onto a target during the end phase of its trajectory, characterized by the combination of the following features: (a) An optical seeker (12) comprises a gyro (18) with a gyro rotor supported, in operation, by compressed air supplied to a gap between a rotor surface and a bearing surface surrounding said rotor surface; (b) An imaging optical system (42) comprising a Cassegrain system, and a detector (40) are provided on said air supported gyro, said imaging optical system being arranged to focus target radiation on said detector (40) and to scan a field of view with a first gyrating scanning motion; (c) The projectile (10), at its front tip, is closed by an optically transparent, planar window (54); (d) The optically transparent window (54) carries a central spike (14); (e) The projectile is provided with tail stabilizing fins (30) and wings (32) in its mid-portion, said wings (32) being controlled by signals from said detector (40) and said gyro (18) through signal processing means (24) and servomotor means (22); and, (f) The projectile (10) is shaped to be driven aerodynamically to make a continuous roll movement and, thereby, to provide a second gyrating scanning motion of said seeker (12).