A precision-guided hypersonic
projectile weapon system. The inventive
system includes a first subsystem for determining a target location and providing data with respect thereto. A second subsystem calculates trajectory to the target based on the data. The
projectile is then launched and guided in flight along the trajectory to the target. In the illustrative application, the
projectile is a
tungsten rod and the first subsystem includes a forward-looking
infrared imaging
system and a
laser range finder. The second subsystem includes a
fire control system. The
fire control system includes an optional
inertial measurement unit and predicts target location. The projectile is mounted in a
missile launched from a platform such as a vehicle. After an initial burn, the
missile launches the projectile while in flight to the target. The
missile is implemented with a
rocket with a
guidance system and a propulsion system. In accordance with the present teachings, the
guidance system includes a
transceiver system mounted on the projectile. The
transceiver system includes a low-power
continuous wave,
millimeter wavelength wave emitter. A system is included at the launch platform for communicating with the projectile. The platform system sends a blinking command to the projectile and measures the round trip
delay thereof to ascertain the range of the projectile. Velocity is determined by conventional Doppler techniques or differentiation.
Azimuth and elevation are then determined by a monopulse antenna on the launch platform. As a consequence, the platform ascertains the location of the projectile and the
impact point thereof. The platform generates a command to the projectile which is received by the projectile and used to actuate control surfaces to adjust the trajectory and
impact point thereof as necessary.