公开(公告)号：US06739556B1

公开(公告)日：2004-05-25

申请号：US10300141

申请日：2002-11-20

申请人： James Leland Langston

发明人： James Leland Langston

IPC分类号： G05D110

CPC分类号： G08G5/0013 ,  B64D45/0015 ,  B64D2045/0055 ,  G08G5/0056

摘要： A method and apparatus for providing an Aircraft Emergency Safety Control System (AESCS) capable of regaining control of an aircraft that may have been lost due to incapacitation of the crew includes an airborne segment, a ground segment, and a communications segment wherein control of the aircraft is removed from the control of unauthorized person(s) onboard the aircraft, and the aircraft is directed to a destination that is considered a safe location for the aircraft given it's status, and to facilitate a reasonably safe emergency landing.

摘要翻译： 一种用于提供能够重新获得由于机组无能力而可能丢失的飞行器的控制的飞行器紧急安全控制系统（AESCS）的方法和装置，包括机载部分，地面部分和通信部分，其中控制 飞机从飞机上的未经授权的人员的控制中被移走，飞机被引导到被认为是飞机的状态的安全位置的目的地，并且促进了相当安全的紧急着陆。

公开(公告)号：US06772055B2

公开(公告)日：2004-08-03

申请号：US10169383

申请日：2002-07-02

申请人： Hans-Ove Hagelin

发明人： Hans-Ove Hagelin

IPC分类号： G05D110

CPC分类号： G05D1/0088 ,  G05B13/0265 ,  G09B9/052

摘要： The invention concerns a system for generating basis for decisions concerning the behavior of a vehicle and/or of a driver of a vehicle. The system comprises a supervising unit (10) which comprises at least one storage member (12). In the storage member (12) there is a set of rules (14) of a particular kind for how the driver of the vehicle and/or the vehicle shall behave in different situations. The system also comprises a user interface (16) and adaptation means (13) arranged to adapt said set of rules such that at least some of the rules (14) with conclusions (24) belonging thereto are suited to form the basis for decisions concerning the behavior of a vehicle and/or of a driver of a vehicle. The invention also concerns a vehicle and a method of generating basis for decisions concerning the behavior of a vehicle and/or of a driver of a vehicle.

摘要翻译： 本发明涉及一种用于产生关于车辆和/或车辆驾驶员的行为的决定的基础的系统。 该系统包括一个包括至少一个存储构件（12）的监督单元（10）。 在存储构件（12）中，存在一组特定类型的规则（14），用于车辆和/或车辆的驾驶员在不同情况下的行为。 该系统还包括用户界面（16）和适配装置（13），其被配置为适应所述规则集，使得属于其的结论（24）的规则（14）中的至少一些适合于形成关于 车辆和/或车辆驾驶员的行为。 本发明还涉及一种用于为车辆和/或车辆驾驶员的行为作出决定的基础的车辆和方法。

公开(公告)号：US06439512B1

公开(公告)日：2002-08-27

申请号：US09645188

申请日：2000-08-24

申请人： Kenneth Edward Hart

发明人： Kenneth Edward Hart

IPC分类号： G05D110

CPC分类号： B64C13/40

摘要： A control system utilizes hydraulic power only to control a fixed-wing aircraft horizontal stabilizer trim control surface with no electrical control devices except for a cockpit pilot/co-pilot initiated 3-position spring-centered toggle trim switch, a backup electrical motor and a standard electronic logic pilot interface. The toggle trim switch controls two solenoid valves which control the operation of a directional control valve. The control system also includes a hydraulic motor, a rate control valve, a blocking-bypass valve, a shutoff valve with an integrated position sensor and a gear set driving an acme threaded output shaft for elevating or lowering the horizontal stabilizer trim control surface on command by the pilot. The control system controls the horizontal stabilizer trim control surface angular displacement rate as a function of angular position by means of a mechanical feedback linkage between the spool of the rate control valve and the horizontal stabilizer trim control surface. The sleeve of the rate control valve has a variable outflow area slot to control the hydraulic flow rate to the motor ports of the hydraulic motor. The horizontal stabilizer trim control surface is automatically stopped at pre-determined maximum-up/maximum-down positions by means of a mechanical feedback linkage between the horizontal stabilizer trim control surface and the spool of the shutoff valve. If the mechanical feedback linkage between the rate control valve spool and the horizontal stabilizer trim control surface malfunctions, the rate control valve automatically reverts to a default fixed flow rate which translates into a corresponding fixed horizontal stabilizer trim control surface angular displacement rate.

摘要翻译： 控制系统仅使用液压动力来控制固定翼飞机水平稳定器调整控制面，没有电气控制装置，除了驾驶舱先导/副驾驶起动的3位弹簧中心的肘节调节开关，备用电动机和 标准电子逻辑导频接口。 拨动装置开关控制两个控制方向控制阀操作的电磁阀。 控制系统还包括液压马达，速率控制阀，阻塞旁通阀，具有集成位置传感器的截止阀和驱动尖端螺纹输出轴的齿轮组，用于根据命令升降水平稳定器调整控制面 由飞行员。 控制系统通过速率控制阀的阀芯与水平稳定器调节控制表面之间的机械反馈联动来控制水平稳定器调整控制表面角位移速率作为角位置的函数。 速率控制阀的套筒具有可变的流出区域槽，用于控制到液压马达的马达端口的液压流量。 水平稳定器调整控制表面通过水平稳定器调整控制表面和截止阀阀芯之间的机械反馈联动自动停止在预定的最大/最大下降位置。 如果速率控制阀阀芯与水平稳定器调节控制表面故障之间的机械反馈联动，速率控制阀自动恢复到默认的固定流量，转换为相应的固定水平稳定器调整控制面角位移速率。

公开(公告)号：US06352223B1

公开(公告)日：2002-03-05

申请号：US09497397

申请日：2000-02-03

申请人： Panxika Larramendy

发明人： Panxika Larramendy

IPC分类号： G05D110

CPC分类号： B64C13/503 ,  G05D1/0808

摘要： The present invention relates to a system for the yaw control of an aircraft fitted with a plurality of engines, the system (SC) comprising in particular a computation unit (16) formulating a command dr for yaw control, dr=Ka.&PHgr;c+Kb.p+Kc.&PHgr;+Kd.r+Ke.&bgr;, on the basis of the controlled roll attitude &PHgr;c, of the roll rate p, of the effective roll attitude &PHgr;, of the yaw rate r, of the sideslip &bgr; and of gains Ka, Kb, Kc, Kd and Ke which are fixed by a device (28). According to the invention, the system (SC) comprises a a device (30) for detecting any fault with an engine of the aircraft, and the device (28) is formed in such a way as to modify the values of the gains Ka, Kd and Ke relating respectively to the controlled roll attitude &PHgr;c, to the yaw rate r and to the sideslip &bgr;, upon the detection by the device (30) of a fault with an engine of the aircraft.

摘要翻译： 本发明涉及一种用于装备有多个发动机的飞行器的偏航控制系统，该系统（SC）特别包括一个计算单元（16），该计算单元（16）制定用于偏航控制的命令dr，Ka =＆amp; + Kb.p + Kc。＆PHgr; + Kd.r + Ke.beta，基于横摆率r的有效倾斜姿态＆Phgr i的滚动速度p的受控滚动姿态＆lt; cgr; c， 的侧片β以及由装置（28）固定的增益Ka，Kb，Kc，Kd和Ke。 根据本发明，系统（SC）包括用于检测飞机发动机的任何故障的装置（30），并且装置（28）形成为改变增益Ka，Kd的值 和Ke分别对应于控制的滚动姿势（PHgr）; c，相对于偏航速度r和侧滑β，在装置（30）检测到飞机发动机的故障时。

公开(公告)号：US06772053B2

公开(公告)日：2004-08-03

申请号：US10269336

申请日：2002-10-11

申请人： Günter D. Niemeyer

发明人： Günter D. Niemeyer

IPC分类号： G05D110

CPC分类号： A61B1/00149 ,  A61B34/30 ,  A61B34/35 ,  A61B34/37 ,  A61B34/70 ,  A61B34/76 ,  A61B90/36 ,  A61B2034/102 ,  A61B2034/305 ,  A61B2090/506 ,  B25J9/1689 ,  G05B2219/40122 ,  G05B2219/45118 ,  H04N13/239 ,  H04N13/246 ,  H04N13/327 ,  H04N2005/2255

摘要： A surgical method and a control system is provided. The surgical method and the control system can advantageously be used in a minimally invasive surgical apparatus. The method includes generating a desired surgical instrument movement command signal. It further includes comparing the desired surgical instrument movement command signal with at least one preset surgical instrument movement limitation. Should the desired surgical instrument command signal transgress the preset surgical instrument movement limitation, the desired surgical instrument movement command signal is restricted to yield a restricted surgical instrument movement command signal. A surgical instrument is then caused to move in response to the restricted surgical instrument movement command signal. The method further provides for haptic feedback on a master control in response to restriction of the desired surgical instrument movement command signal.

摘要翻译： 提供外科手术方法和控制系统。 手术方法和控制系统可有利地用于微创外科手术装置中。 该方法包括产生期望的外科器械移动指令信号。 其还包括将期望的手术器械运动指令信号与至少一个预设的手术器械移动限制进行比较。 如果期望的手术器械指令信号超过预设的手术器械运动限制，则期望的手术器械移动指令信号被限制以产生受限的手术器械移动指令信号。 然后使手术器械响应于限制的手术器械移动指令信号而移动。 该方法还响应于期望的外科器械移动指令信号的限制，提供对主控制器的触觉反馈。

公开(公告)号：US06615115B1

公开(公告)日：2003-09-02

申请号：US09620870

申请日：2000-07-21

申请人： Yin-Chun Huang

发明人： Yin-Chun Huang

IPC分类号： G05D110

CPC分类号： H04N1/1013 ,  H04N1/1026 ,  H04N2201/046

摘要： A control method for removing scanning discontinuity in scanners. The relationship between a driving motor and an elastic body such as a leather belt or a steel cable linked to the chassis inside a scanner is investigated so that time constants for achieving system stability are found. Through setting the time constants, the forwarding and reversing motion of the chassis is controlled so that scanning discontinuity due to stopping and restarting is reduced.

摘要翻译： 扫描仪扫描不连续的控制方法。 研究驱动电动机与连接在扫描仪内部的底盘的皮带或钢缆的弹性体之间的关系，从而发现实现系统稳定性的时间常数。 通过设置时间常数，控制机箱的转发和反转运动，从而减少由于停止和重启而导致的扫描不连续。

公开(公告)号：US06493608B1

公开(公告)日：2002-12-10

申请号：US09288068

申请日：1999-04-07

申请人： Gunter D. Niemeyer

发明人： Gunter D. Niemeyer

IPC分类号： G05D110

CPC分类号： A61B1/00149 ,  A61B34/30 ,  A61B34/35 ,  A61B34/37 ,  A61B34/70 ,  A61B34/76 ,  A61B90/36 ,  A61B2034/102 ,  A61B2034/305 ,  A61B2090/506 ,  B25J9/1689 ,  G05B2219/40122 ,  G05B2219/45118 ,  H04N13/239 ,  H04N13/246 ,  H04N13/327 ,  H04N2005/2255

摘要： A surgical method and a control system is provided. The surgical method and the control system can advantageously be used in a minimally invasive surgical apparatus. The method includes generating a desired surgical instrument movement command signal. It further includes comparing the desired surgical instrument movement command signal with at least one preset surgical instrument movement limitation. Should the desired surgical instrument command signal transgress the preset surgical instrument movement limitation, the desired surgical instrument movement command signal is restricted to yield a restricted surgical instrument movement command signal. A surgical instrument is then caused to move in response to the restricted surgical instrument movement command signal. The method further provides for haptic feedback on a master control in response to restriction of the desired surgical instrument movement command signal.

摘要翻译： 提供外科手术方法和控制系统。 手术方法和控制系统可有利地用于微创外科手术装置中。 该方法包括产生期望的外科器械移动指令信号。 其还包括将期望的手术器械运动指令信号与至少一个预设的手术器械移动限制进行比较。 如果期望的手术器械指令信号超过预设的手术器械移动限制，则期望的手术器械移动指令信号被限制以产生受限的手术器械移动指令信号。 然后使手术器械响应于限制的手术器械移动指令信号而移动。 该方法还响应于期望的外科器械移动指令信号的限制，提供对主控制器的触觉反馈。