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公开(公告)号：US4129268A
公开(公告)日：1978-12-12
申请号：US503838
申请日：1965-10-23
申请人： Willis F. Tibbetts
发明人： Willis F. Tibbetts
CPC分类号： G01C19/025 , F41G7/36 , F42B15/01
摘要： 1. A rocket comprising a rear section including a motor, a forward war head section, an intermediate trajectory control section, and a rotatable connection between said control and motor sections, a gyroscope and a gas generator mounted within said control section, the generator ahead of the gyroscope, said gas generator including ignition means, a first nozzle operable to deliver a wheel-driving gas stream to the wheel of said gyroscope, and a second nozzle operable to deliver an upward thrust in assistance of the flight of said rocket, the thrust being applied approximately in the zone of the center of gravity of said rocket, means operable in response to a predetermined set-back force exerted on said rocket during its launch to engage and support said wheel against said force only during the existence of said force, gyroscope caging means, and means to release said caging means in response to the operation of said generator.
摘要翻译： 1.一种火箭，包括后部，包括马达，前向战头部分，中间轨迹控制部分以及所述控制部分和马达部分之间的可旋转连接，安装在所述控制部分内的陀螺仪和气体发生器， 所述气体发生器包括点火装置，可操作以将车轮驱动气流输送到所述陀螺仪的车轮的第一喷嘴;以及第二喷嘴，所述第二喷嘴可操作以在所述火箭的飞行协助下传递向上的推力， 推力大致施加在所述火箭重心的区域中，该装置可在响应于在其发射期间施加在所述火箭上的预定的后退力而操作，仅在所述力的存在期间接合并支撑所述轮抵抗所述力 ，陀螺仪闭合装置，以及响应于所述发生器的操作释放所述笼式装置的装置。
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公开(公告)号：US3721410A
公开(公告)日：1973-03-20
申请号：US3721410D
申请日：1962-08-29
申请人： US NAVY
发明人： ANSPACHER W
CPC分类号： G01C11/025 , F41G3/02 , F42B12/365 , F42B15/08
摘要： 1. A reconnaissance system capable of scanning an inaccessible target area and relaying the information to an observation point where it is displayed for visual observation comprising an infrared transducer means for converting detected infrared radiations into electrical signals proportional to the detected infrared radiations, transmitting means connected to said transducer means for transmitting electrical signals, rotating projectile means rotating at a predetermined rate enclosing said transmitting means and having said transducer means fixedly attached to the outer periphery of the projectile for scanning in a helical path the target area in a fixed rotating relationship with the projectile, at a rate equal to the rotating rate of said projectile receiving means for receiving and demodulating said electrical signals, and visual display means connected to said receiving means for converting electrical signals into a visual representation of the target area.
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公开(公告)号：US4309003A
公开(公告)日：1982-01-05
申请号：US117699
申请日：1980-02-01
申请人： William B. McLean
发明人： William B. McLean
CPC分类号： F41G7/2293 , F41G7/2213 , F41G7/2253
摘要： A free spinning gyroscope is provided which has a spin axis, together with precession means for precessing the gyroscope. In addition, means are provided for detecting an electromagnetic field of energy and adapted to generate signals indicative of misalignment of the gyroscope spin axis with the energy field. Means are provided for utilizing the generated signals to directly control the precessing means to align the gyroscope spin axis with the electromagnetic field of energy.
摘要翻译： 提供了具有旋转轴的自由旋转陀螺仪，以及进动陀螺仪的进动装置。 另外，提供了用于检测能量的电磁场并适于产生指示陀螺仪旋转轴与能量场的未对准的信号的装置。 提供了用于利用所产生的信号来直接控制进动装置以使陀螺仪旋转轴与能量的电磁场对准的装置。
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公开(公告)号：US4262596A
公开(公告)日：1981-04-21
申请号：US952427
申请日：1978-10-18
申请人： Michel Allier , Didier Lursat
发明人： Michel Allier , Didier Lursat
CPC分类号： F42B12/14
摘要： A overhead attack missile for targets of little movement such as tanks or firing turrets is described. It comprises: at least one hollow charge, with a unidirectional radial action possessing a pyrotechnic dissymmetry means such as the off-centering of the detonator of the charge to preserve the straightness of the burst despite the movement of the missile and a guidance means to bring the missile, at the end its course, overhead of the target. The invention is applied to any stabilized or unmanned aerial weapons carrying war heads.
摘要翻译： 描述了对于诸如坦克或发射炮塔之类的小动作目标的高空攻击导弹。 它包括：至少有一个中空电荷，具有单向径向作用，具有烟火不对称的手段，例如导弹的雷管的偏心，以保持爆发的平直度，尽管导弹的移动和引导装置带来 导弹，到最后的路线，目标的开销。 本发明适用于携带战头的任何稳定的或无人驾驶的空中武器。
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5.发明授权Feedback PDM encoder and method for actuating a pneumatic actuator with a digital autopilot 失效反馈PDM编码器和用于启动具有数字自动驾驶仪的气动执行器的方法
公开(公告)号：US4033525A
公开(公告)日：1977-07-05
申请号：US638476
申请日：1975-12-08
申请人： John P. Leonard , Robert E. Yates
发明人： John P. Leonard , Robert E. Yates
CPC分类号： F41G7/301 , G05D1/0202 , G05D3/18
摘要： A feedback PDM encoder and method is presented which permits utilization ofneumatic pulse duration modulation (PDM) actuators with potentiometer position pickoffs in a digital autopilot loop. The actuator is directly driven by a signal derived in the digital autopilot which is in the pulse duration modulation (PDM) format. This signal is derived within the autopilot digital computer using conventional digital techniques. Analog feedback from the potentiometer which indicates angular excursion of the actuator is formatted into a PDM format. This method yields all signals necessary to operate the actuator in a closed loop missile control system.
摘要翻译： 提出了一种反馈PDM编码器和方法，其允许在数字自动驾驶仪环路中利用具有电位计位置传感器的气动脉冲持续时间调制（PDM）致动器。 致动器由在数字自动驾驶仪中得到的信号直接驱动，该信号处于脉冲宽度调制（PDM）格式。 该信号是使用传统的数字技术在自动驾驶仪数字计算机内导出的。 来自电位计的模拟反馈表示执行器的角度偏移被格式化为PDM格式。 该方法产生在闭环导弹控制系统中操作执行器所需的所有信号。
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公开(公告)号：US3758052A
公开(公告)日：1973-09-11
申请号：US3758052D
申请日：1969-07-09
申请人： US NAVY
发明人： MC ALEXANDER R , STOUT L
CPC分类号： F42B15/00 , F42C13/047
摘要： The present invention is a gun system which utilizes rocket assisted projectiles and accurately controls their placement. The projectile is fired by a gun and actual trajectory variables are compared in a computer with desired trajectory conditions. If there is a difference, the firing time of the rocket is altered to make the actual trajectory variable correspond to the desired condition. A radar system is utilized by the computer to obtain the trajectory information. A transmitter is connected to the computer to send the firing signal to a receiver mounted in the projectile.
摘要翻译： 本发明是利用火箭辅助射弹并准确地控制其放置的枪系统。 射弹由枪射击，实际轨迹变量在具有所需轨迹条件的计算机中进行比较。 如果存在差异，则改变火箭的点火时间，使实际的轨迹变量对应于所需条件。 计算机利用雷达系统获得轨迹信息。 发射器连接到计算机以将发射信号发送到安装在射弹中的接收器。
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公开(公告)号：US4307855A
公开(公告)日：1981-12-29
申请号：US117598
申请日：1980-02-01
申请人： William B. McLean
发明人： William B. McLean
CPC分类号： F41G7/2253 , F41G7/2213 , F41G7/2293
摘要： A free spinning gyroscope is provided which has a spin axis, together with precession means for precessing the gyroscope. In addition, means are provided for detecting an electromagnetic field of energy and adapted to generate signals indicative of misalignment of the gyroscope spin axis with the energy field. Means are provided for utilizing the generated signals to directly control the precessing means to align the gyroscope spin axis with the electromagnetic field of energy.
摘要翻译： 提供了具有旋转轴的自由旋转陀螺仪，以及进动陀螺仪的进动装置。 另外，提供了用于检测能量的电磁场并适于产生指示陀螺仪旋转轴与能量场的未对准的信号的装置。 提供了用于利用所产生的信号来直接控制进动装置以使陀螺仪旋转轴与能量的电磁场对准的装置。
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公开(公告)号：US4037806A
公开(公告)日：1977-07-26
申请号：US397674
申请日：1964-09-16
CPC分类号： G05D1/12 , F41G7/2213 , F41G7/222 , F41G7/2253 , F41G7/2293 , F42B10/64 , F42B15/01 , G05D1/108
摘要： This invention relates to a servocontrol system for a weapon such as a missile which is a shoulder-launched, infrared-homing, guided missile which provides frontline troops with effective air defense against low altitude enemy aircraft. The weapon, described herein for purposes of illustration, consists of a missile and launcher combination which can be readily transported and operated within the normal environments associated with ground forces in a combat area. To meet the size, weight, and performance requirements, the missile achieves passive homing guidance by using a space-stabilized, infrared-seeking-head control system to generate guidance signals for a single-channel, variable-incidence wing control system working in conjunction with a rolling airframe.
摘要翻译： 本发明涉及一种用于诸如导弹的武器的伺服控制系统，该导弹是肩膀发射的红外归巢导弹，为前线部队提供对低空敌机的有效防空。 为了说明的目的，这里描述的武器包括导弹和发射器组合，其可以在与作战区域中的地面力相关联的正常环境中容易地运输和操作。 为了满足大小，重量和性能要求，导弹通过使用空间稳定的红外搜索头控制系统来实现被动归位指导，为单通道，可变入射翼控制系统生成指导信号 与滚动的机身。
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公开(公告)号：US4026498A
公开(公告)日：1977-05-31
申请号：US602040
申请日：1975-08-05
申请人： Daniel H. Platus
发明人： Daniel H. Platus
CPC分类号： F41G7/34 , G05D1/0808 , G05D1/108
摘要： A sensor system that measures flight motions with respect to a classical Euler angle system of coordinates by aligning itself with the plane of total angle of attack via a pendulum mass. The system permits a simple determination of lift and drag for a spinning vehicle at angle of attack whereby the measurements are used as inputs to a flight control system to control the motions of the spinning vehicle.
摘要翻译： 传感器系统，通过摆锤质量与自身与总迎角平面对准，测量相对于古典欧拉角坐标系的飞行运动。 该系统允许在迎角处简单地确定纺纱车辆的升力和阻力，由此将测量值用作飞行控制系统的输入以控制旋转车辆的运动。
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公开(公告)号：US3724379A
公开(公告)日：1973-04-03
申请号：US3724379D
申请日：1966-10-05
申请人： US AIR FORCE
发明人： DAVIS D
CPC分类号： F42B12/204 , F42B15/08 , F42B15/34
摘要： An improved air-to-surface missile having a warhead which is confined solely to the lower half of the missile, and this half contains all the fragments which would normally be distributed throughout both halves of the missile. An upper casing portion need not be employed except to maintain symmetry and aerodynamic stability of the missile as a whole. In order to offset the slewing effect of the fragment pattern at the target on account of a low angle of approach, the fragmented lower surface of the warhead is flattened as it extends toward the rear end and is also curved upwardly so as to approach the longitudinal axis of the missile which contains the warhead.
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