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81. 发明授权

US2711856A Bombing computer 失效
标题翻译：轰炸电脑
公开(公告)号：US2711856A
公开(公告)日：1955-06-28
申请号：US59816245
申请日：1945-06-07
申请人： GRAY JOHN W , MACRAE JR DUNCAN
发明人： GRAY JOHN W , MACRAE JR DUNCAN
IPC分类号： G06G7/80
CPC分类号： G06G7/80

82. 发明授权

US2686636A Curved course predictor 失效
标题翻译：弯曲的课程预测
公开(公告)号：US2686636A
公开(公告)日：1954-08-17
申请号：US67935346
申请日：1946-06-26
申请人： BELL TELEPHONE LABOR INC
发明人： EMORY LAKATOS , OCH HENRY G
IPC分类号： F41G5/08 , G06G7/80
CPC分类号： F41G5/08 , G06G7/80

83. 发明授权

US2658674A Artillery computer having deck tilt and gun parallax correction factors 失效
标题翻译：火炮计算机具有甲板倾斜和炮视差校正因素
公开(公告)号：US2658674A
公开(公告)日：1953-11-10
申请号：US57762345
申请日：1945-02-13
申请人： BELL TELEPHONE LABOR INC
发明人： SIDNEY DARLINGTON , LUNDSTROM ALEXIS A
IPC分类号： F41G5/14 , G06G7/80
CPC分类号： F41G5/14 , G06G7/80

84. 发明授权

US2545655A Computer 失效
公开(公告)号：US2545655A
公开(公告)日：1951-03-20
申请号：US58750045
申请日：1945-04-10
IPC分类号： G06G7/80
CPC分类号： G06G7/80

85. 发明申请

US20150310603A1 SYSTEM, METHOD, AND COMPUTER PROGRAM PRODUCT FOR INDICATING HOSTILE FIRE 有权
公开(公告)号：US20150310603A1
公开(公告)日：2015-10-29
申请号：US13804513
申请日：2013-03-14
申请人： LOCKHEED MARTIN CORPORATION
发明人： Stephen C. Moraites , Shawn McPhail , Donald Sobiski
IPC分类号： G06T7/00 , H04N7/18 , G06T7/20 , H04N5/232 , H04N5/44 , G01J5/00 , H04N5/33
CPC分类号： G06T7/20 , G01B11/00 , G01J5/00 , G01J2005/0077 , G06G7/80 , G06K9/0063 , G06T2207/10048 , G06T2207/30212 , G06T2207/30241 , H04N5/23296 , H04N5/33 , H04N5/44 , H04N7/183
摘要： A network for indicating and communicating detection of hostile fire, and systems, methods, and computer program products thereof. Hostile fire is optically detected and identified at a first vehicle and such identification is transmitted from the first vehicle to one or more other vehicles in the network. Data regarding hostile fire directed at the first vehicle can be stored at one or more of the other vehicles and even retransmitted to other vehicles or base stations.

86. 发明授权

US4047014A Coordinate converter 失效
标题翻译：坐标转换器
公开(公告)号：US4047014A
公开(公告)日：1977-09-06
申请号：US672893
申请日：1976-04-02
申请人： Steven Morrison , George A. Williams
发明人： Steven Morrison , George A. Williams
IPC分类号： G06G7/22 , G06G7/80
CPC分类号： G06G7/80 , G06G7/22
摘要： An electronically controlled coordinate converter for transforming vectors from a first coordinate system to a second coordinate system through an input angle is provided using a harmonic oscillator which is responsive to an oscillation angle control signal having a discontinuity or transition point wherein an incremental change in the input angle at a predetermined value causes a step function in the duration of said oscillation angle control signal. The discontinuity in the oscillation angle control signal is eliminated by control circuits within a selected range of input angles where the error effects due to transformations on either side of the discontinuity are avoided. Another feature of the invention is that the discontinuity in the oscillation angle control signal may be shifted away from or in response to a previous vector transformation having an input angle close to the discontinuity to avoid recurrent vector transformations on either side of the oscillation angle control signal discontinuity due to slight incremental fluctuations in the input angle.
摘要翻译：使用谐波振荡器提供用于通过输入角将矢量从第一坐标系变换到第二坐标系的电子控制坐标转换器，其响应于具有不连续或转变点的振荡角控制信号，其中输入的增量变化在预定值处的角度在所述振荡角度控制信号的持续时间内产生阶跃函数。振荡角度控制信号中的不连续性由输入角度选定范围内的控制电路消除，其中避免了由于不连续性的任一侧上的变换导致的误差效应。本发明的另一个特征是振荡角度控制信号的不连续性可以偏离或响应于具有接近于不连续性的输入角的先前矢量变换，以避免在振荡角度控制信号的任一侧上的反复向量变换由于输入角度的轻微增量波动引起的不连续性。

87. 发明授权

US4017718A Altitude control system for drones 失效
标题翻译：无人机高度控制系统
公开(公告)号：US4017718A
公开(公告)日：1977-04-12
申请号：US656703
申请日：1976-02-09
申请人： Robert John Gerrity , Clarence Dwight Wandrey , Benjamin Howard Dolbin, deceased
发明人： Robert John Gerrity , Clarence Dwight Wandrey , Benjamin Howard Dolbin, deceased
IPC分类号： G05D1/06 , G06G7/22 , G06G7/78 , G06G7/80
CPC分类号： G06G7/80 , G05D1/0607 , G06G7/22 , G06G7/78
摘要： An approximation is made in the equation for the desired vertical profile command signal to control the altitude of a drone traveling towards a target such that simple analog circuitry may be utilized instead of complicated computers.
摘要翻译：对于期望的垂直剖面命令信号的方程式进行近似，以控制向目标行进的无人机的高度，从而可以利用简单的模拟电路而不是复杂的计算机。

88. 发明授权

US4017716A Method and apparatus for directing an observation member 失效
标题翻译：用于引导观察构件的方法和装置
公开(公告)号：US4017716A
公开(公告)日：1977-04-12
申请号：US652885
申请日：1976-01-27
申请人： Carl Torbern Teiling
发明人： Carl Torbern Teiling
IPC分类号： G06G7/80
CPC分类号： G06G7/80
摘要： Two systems are disclosed in which a pointer is directed towards a moving target over a predetermined time interval. Angular information is derived from the pointer during this time interval to generate signals indicative of the distance of the object from the pointer. During a second time interval, the pointer is automatically directed towards the moving object by use of the information derived during the first time interval.
摘要翻译：公开了两个系统，其中指针在预定时间间隔内被指向移动目标。角度信息在该时间间隔期间从指针导出，以产生指示对象与指针的距离的信号。在第二时间间隔期间，通过使用在第一时间间隔期间导出的信息，指针自动地指向移动对象。

89. 发明授权

US3860791A Deflection angle plotter 失效
标题翻译：偏转角度计
公开(公告)号：US3860791A
公开(公告)日：1975-01-14
申请号：US71416768
申请日：1968-03-13
申请人： US NAVY
发明人： HEADLE JR HERBERT W
IPC分类号： G06G7/80
CPC分类号： G06G7/80
摘要： A deflection angle plotter is provided which replaces the conventional set of plotting curves by a pair of rolled tapes both of which may be extended and retracted and are pivotable at their rolled end and pinned together at the other end. One tape is slotted near the end, this slot accommodates a pin mounted on the other tape. The tape carrying the pin is slidable along the ordinate of the plotter at its rolled end. Target range from own ship is introduced by displacement along the ordinate of the tape carrying the pin while the direction and amount of extension of that tape represents target course and distance to acquisition. Torpedo course and distance to acquisition are represented by the nonslidable tape. Inputs of target course, target range, target speed, torpedo pre-enable speed, torpedo post-enable speed and torpedo enable run distance into a plotter control circuit provide, through appropriate potentiometers and other conventional circuit components, meter readings of range, angle on the bow, target bearing rate, deflection angle and torpedo run time in the rapid solution of a plurality of problems each having a plurality of different parameters.
摘要翻译：提供了一种偏转角绘图仪，其通过一对卷筒带代替传统的一组绘图曲线，两个卷筒带可以伸展和缩回，并且可以在其卷绕端枢转并在另一端固定在一起。一个磁带在端部附近开槽，该插槽容纳安装在另一个磁带上的引脚。承载销的带可沿着卷轴端的绘图机的纵坐标滑动。本船的目标范围通过位于沿着带子的带状位置引入，而该带的延伸方向和数量代表目标路线和到达采集距离。鱼雷课程与拍摄距离由不可分割的胶带代表。目标行程，目标范围，目标速度，鱼雷预启动速度，鱼雷后启用速度和鱼雷的输入使得到绘图仪控制电路的运行距离通过适当的电位器和其他常规电路组件提供范围的读数，角度在具有多个不同参数的多个问题的快速解决中，弓，目标承载率，偏转角和鱼雷运行时间。

90. 发明授权

US3784800A Systems for surveying and correcting trajectories 失效
标题翻译： TRAJECTORIES调查和校正系统
公开(公告)号：US3784800A
公开(公告)日：1974-01-08
申请号：US3784800D
申请日：1972-05-26
申请人： EQUIPMENTS NAVIGATION AERODROM
发明人： WILLOTEAUX G
IPC分类号： F41G7/22 , F41G7/30 , F41G7/34 , G01S13/93 , G05D1/04 , G05D1/12 , G06G7/20 , G06G7/70 , G06G7/78 , G06G7/80 , G08G5/00 , G09B9/08
CPC分类号： G08G5/0078 , F41G7/22 , F41G7/301 , F41G7/343 , G01S13/9303 , G05D1/12 , G06G7/20 , G06G7/70 , G06G7/78 , G06G7/80 , G08G5/0052 , G09B9/08
摘要： A system for controlling the trajectory of a moving body such as an aircraft or missile moving in the vicinity of one or more relevant objects which may be moving or stationary. The trajectory is required to fulfil certain imperatives such that the body following it either avoids the relevant object by at least a specified distance or the imperatives may require the body to hit or come within at least a specified distance of the object. The system calculates the distance between the body and object and by taking account of the speeds and direction of each simulates a series of hypothetical trajectories diverging on either side of the actual trajectory until a hypothetical trajectory is determined which satisfies the imperatives, the system then instructs the body''s controls to change the linear and/or angular speed thereof so that the aircraft follows the latter trajectory.
摘要翻译：一种用于控制在可移动或静止的一个或多个相关物体附近移动的飞行器或导弹等移动体的轨迹的系统。轨迹需要履行某些要求，使得跟随其后的身体避免至少指定距离的相关对象，或者必要性可能要求身体在物体至少指定距离内进入或进入。系统计算身体和物体之间的距离，并考虑到每个人的速度和方向模拟一系列在实际轨迹的任一侧发散的假想轨迹，直到确定满足命令的假设轨迹，系统然后指示身体的控制以改变其线性和/或角速度，使得飞机遵循后一轨迹。

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