发明名称 Pitch-yaw stabilization system
摘要 A laser beamrider projectile having a lens system and a four-quadrant photodiode detector, which eliminates the need for rate gyros in the projectile to provide stabilization. When the projectile is aligned with the beam, the beam image is centered on the intersection of the four quadrants of the detector, and when the projectile pitch or yaw angle deviates, more light strikes one or two of the quadrants than the others. Comparison circuitry connected to the detector outputs provides one error signal proportional to pitch angle deviation and another error signal proportional to yaw angle deviation. These signals are usable by the projectile flight control system to eliminate oscillation in pitch and yaw. Preferably, an angle rate signal is also supplied to the stabilization system in addition to or instead of the angle deviation signal. The full specification must be consulted for an understanding of the invention.
申请公布号 US4021007(A) 申请公布日期 1977.05.03
申请号 US19740514243 申请日期 1974.10.11
申请人 NORTHROP CORPORATION 发明人 COXE, FRANK S.
分类号 F41G7/26;(IPC1-7):F41G7/14;F41G9/00;F41G7/00 主分类号 F41G7/26
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