公开(公告)号：US20080195259A1

公开(公告)日：2008-08-14

申请号：US11672603

申请日：2007-02-08

申请人： Terry L. Davis ,  Scott L. Pelton

发明人： Terry L. Davis ,  Scott L. Pelton

IPC分类号： G06F19/00

CPC分类号： H04B3/548 ,  H04B2203/5441 ,  H04B2203/5458 ,  H04B2203/547

摘要： Methods and systems for transmitting power and digital communication are provided. The method includes communicatively coupling a broadband over power line interface unit to a power conductor of a temporary power cable, communicatively coupling the broadband over power line interface unit to a network access point, electrically coupling the power conductor to a vehicle power receptacle, and transmitting network data between the network and the vehicle, and powering the vehicle simultaneously through the power conductor.

摘要翻译： 提供了发送功率和数字通信的方法和系统。 该方法包括将电力线接口单元上的宽带通信耦合到临时电力电缆的电力导体，将通过电力线接口单元的宽带通信地耦合到网络接入点，将电力导体电连接到车辆电源插座，以及发送 网络和车辆之间的网络数据，以及通过电源导体同时为车辆供电。

公开(公告)号：US07893557B2

公开(公告)日：2011-02-22

申请号：US11672603

申请日：2007-02-08

申请人： Terry L. Davis ,  Scott L. Pelton

发明人： Terry L. Davis ,  Scott L. Pelton

IPC分类号： G06F19/00

CPC分类号： H04B3/548 ,  H04B2203/5441 ,  H04B2203/5458 ,  H04B2203/547

摘要： Methods and systems for transmitting power and digital communication are provided. The method includes communicatively coupling a broadband over power line interface unit to a power conductor of a temporary power cable, communicatively coupling the broadband over power line interface unit to a network access point, electrically coupling the power conductor to a vehicle power receptacle, and transmitting network data between the network and the vehicle, and powering the vehicle simultaneously through the power conductor.

摘要翻译： 提供了发送功率和数字通信的方法和系统。 该方法包括将电力线接口单元上的宽带通信耦合到临时电力电缆的电力导体，将通过电力线接口单元的宽带通信地耦合到网络接入点，将电力导体电连接到车辆电源插座，以及发送 网络和车辆之间的网络数据，以及通过电源导体同时为车辆供电。

公开(公告)号：US4956780A

公开(公告)日：1990-09-11

申请号：US386874

申请日：1989-07-27

申请人： Mithra M. K. V. Sankrithi ,  Scott L. Pelton

发明人： Mithra M. K. V. Sankrithi ,  Scott L. Pelton

IPC分类号： G05D1/06

CPC分类号： G05D1/0676

摘要： This invention provides a flare control modification for pilot-in-the-loop aircraft maneuver command electronic flight control systems. During flare pilot pitch control inputs are interpreted as incremental flight path angle commands above a reference flight path angle (nominally a -3.degree. glideslope). The flare control modification allows conventional piloting technique (i.e., pitch controller pull-and-hold) to be used during flare, while retaining the benefits of the maneuver command system masking effects of gusts, winds, windshear, and variations in airplane weight, balance, and aerodynamic configuration.

摘要翻译： 本发明提供了一种用于先导式在线飞行器机动指令电子飞行控制系统的火炬控制修改。 在火炬飞行时，俯仰控制输入被解释为高于参考飞行路径角度（标称为-3°滑坡）的增量飞行路径角度命令。 火炬控制修改允许在火炬期间使用常规的驾驶技术（即俯仰控制器拉拽和保持），同时保持机动指令系统掩盖了阵风，风，风切变和飞机重量，平衡变化的效果 ，和空气动力学配置。

公开(公告)号：US5036469A

公开(公告)日：1991-07-30

申请号：US319255

申请日：1989-03-02

申请人： Scott L. Pelton

发明人： Scott L. Pelton

IPC分类号： B64C13/18 ,  B64D45/04 ,  G05D1/06

CPC分类号： G05D1/0676

摘要： This invention provides a flare control modification for pilot-in-the-loop aircraft maneuver command electronic flight control systems. During flare, pilot pitch control inputs are interpreted as incremental pitch attitude commands. The flare control modification allows conventional piloting technique (i.e., pitch controller pull-and-hold) to be used during flare, while retaining the benefits of maneuver command system masking effects of gusts, winds, wind shear, and variations in airplane weight, balance, and aerodynamic configuration.

公开(公告)号：US5003305A

公开(公告)日：1991-03-26

申请号：US490007

申请日：1990-03-06

申请人： Brian D. Kelly ,  Scott L. Pelton

发明人： Brian D. Kelly ,  Scott L. Pelton

IPC分类号： G01C23/00 ,  G05D1/06

CPC分类号： G05D1/0607 ,  G01C23/00

摘要： A flight path angle symbol is positioned on an aircraft attitude display indicator as a function of either a measured flight path angle or a flight path angle commanded by the pilot. When the aircraft is operating within a selected airspeed, angle of attack, pitch attitude or load factor range, or the difference between measured flight path angle and commanded flight path angle is within a selected range, the symbol is positioned on the display as a function of commanded flight path angle. However when the aircraft is operating outside any of these ranges, the symbols is positioned on the display as a function of the measured flight path angle. To avoid a rapid jump in symbol position when transitioning between measured and commanded flight path angle displays, a phase lag filter is used to attenuate and lag the symbol positioning signal.

摘要翻译： 作为飞行员指挥的测量的飞行路径角度或飞行路径角度的函数，飞行路径角度符号位于飞行器姿态显示指示器上。 当飞行器在所选择的空速内操作时，迎角，俯仰姿态或载荷因子范围，或测量飞行路径角与指令飞行路径角之间的差在一个选定的范围内，该符号位于显示器上作为一个功能 指挥的飞行路径角度。 然而，当飞行器在任何这些范围之外操作时，符号作为测量的飞行路径角度的函数被定位在显示器上。 为了避免在测量和命令的飞行路径角度显示之间转换时符号位置的快速跳跃，使用相位滞后滤波器来衰减并延迟符号定位信号。