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    • 3. 发明申请
    • Determination of Integrity of Incoming Signals of Satellite Navigation System
    • 卫星导航系统进入信号完整性的确定
    • US20150116147A1
    • 2015-04-30
    • US14068218
    • 2013-10-31
    • Thomas H. Jaeckle
    • Thomas H. Jaeckle
    • G01S19/21
    • G01S19/215
    • A system and method for testing the integrity of signals incoming to a satellite navigation system. The method is implemented with an array of antenna elements, and a receiver connected to each antenna element. The receivers simultaneously and continuously make measurements on all tracked signals. Each receiver measures the carrier phase of an incoming signal. Based on the carrier phase differences between antenna elements and the distance between them, the azimuth and elevation of the signal source can be calculated. This measured angle of arrival can then be compared to an expected angle of arrival to determine if the signal source is legitimate. The system and method can be also applied to determining the angle of arrival of sources of interference, and to mitigating the effects of both illegitimate and interfering signals.
    • 一种用于测试进入卫星导航系统的信号完整性的系统和方法。 该方法由天线元件阵列和连接到每个天线元件的接收器来实现。 接收机同时并连续地对所有跟踪的信号进行测量。 每个接收机测量输入信号的载波相位。 基于天线元件之间的载波相位差和它们之间的距离,可以计算信号源的方位角和高程。 然后将该测量的到达角度与预期的到达角度进行比较,以确定信号源是否合法。 该系统和方法还可以用于确定干扰源的到达角度,并减轻非法和干扰信号的影响。
    • 5. 发明授权
    • Autonomous stratospheric airship
    • 自主平流层飞艇
    • US06386480B1
    • 2002-05-14
    • US09247878
    • 1999-02-15
    • William D. PerryThomas H. JaeckleLawrence E. EpleyAllan B. Black
    • William D. PerryThomas H. JaeckleLawrence E. EpleyAllan B. Black
    • B64B2900
    • B64B1/06B64B1/24B64B1/60
    • An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted within the bull and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.
    • 包括一个包含设备舱,前后气缸,前后空气管理子系统,推进系统和控制系统的船体的自主平流层飞艇。 飞艇还包括一个再生太阳能发电和存储子系统,可以实现日夜和夜间的动力。 此外,飞艇的控制系统可以在选定的航路点之间或沿着特定的视线进行自主运行。 飞艇使用的太阳能阵列内部安装在公牛和gimballed内,以提供最大的收集效率,并且不妨碍飞艇的空气动力学特性。 还公开了在船体外部承载设备舱时,利用替代太阳能阵列控制和镇流器管理系统的飞艇的大大简化和略微可控的版本。
    • 6. 发明授权
    • Autonomous stratospheric airship
    • 自主平流层飞艇
    • US06354535B1
    • 2002-03-12
    • US09661175
    • 2000-09-13
    • William D. PerryThomas H. JaeckleLawrence E. EpleyAllan B. Black
    • William D. PerryThomas H. JaeckleLawrence E. EpleyAllan B. Black
    • B64B2900
    • B64B1/60B64B1/06B64B1/24
    • An autonomous stratospheric airship comprising a hull which contains an equipment bay, forward and aft ballonets, forward and aft air management sub-systems, a propulsion system, and a control system is described. The airship also comprises a regenerative solar energy power and storage sub-system which allows powered daytime and nighttime operations. Further, the control system of the airship enables autonomous operation between selected waypoints or along a specified line of sight. The solar arrays utilized by the airship are internally mounted and gimballed so as to provide maximum collection efficiency and not impede the aerodynamic profile of the airship. A greatly simplified and slightly less controllable version of the airship, which makes use of alternative solar array control and ballast management systems, while carrying the equipment bay on the exterior of the hull, is also disclosed.
    • 包括一个包含设备舱,前后气缸,前后空气管理子系统,推进系统和控制系统的船体的自主平流层飞艇。 飞艇还包括一个再生太阳能发电和存储子系统,可以实现日夜和夜间的动力。 此外,飞艇的控制系统可以在选定的航路点之间或沿着特定的视线进行自主运行。 飞艇使用的太阳能阵列是内部安装的,并且是gimballed的,以提供最大的收集效率,并且不妨碍飞艇的空气动力学特性。 还公开了在船体外部承载设备舱时,利用替代太阳能阵列控制和镇流器管理系统的飞艇的大大简化和略微可控的版本。
    • 7. 发明授权
    • Micropower DC voltage indicator
    • 微功率直流电压指示器
    • US4614940A
    • 1986-09-30
    • US790613
    • 1985-10-21
    • Thomas H. Jaeckle
    • Thomas H. Jaeckle
    • G01R19/165G01R19/155G08B21/20G08B21/00G09G3/18H03B5/12
    • G08B21/185G01R19/155Y10S331/03
    • A micropower DC voltage indicator is provided that is a two terminal device with a very high input impedance. An oscillator circuit is provided by a series of inverters, such as metal-oxide semiconductors (MOS) with the power inputs connected in parallel. A suitable RC circuit connects the output of one MOS inverter to the input of another MOS inverter, otherwise the output of each MOS inverter connects directly to the input of the next MOS inverter. Across one of the MOS inverters is connected a liquid crystal display which indicates if a DC voltage within a specific range is applied to the two terminals of the DC voltage indicator. The two terminal inputs to the oscillator circuit have a very high impedance and operate over a fairly broad DC voltage range.
    • 提供了一个微功率直流电压指示器,它是具有非常高的输入阻抗的双端子器件。 振荡电路由一系列逆变器提供,例如金属氧化物半导体(MOS),并联电源输入。 一个合适的RC电路将一个MOS反相器的输出连接到另一个MOS反相器的输入,否则每个MOS反相器的输出直接连接到下一个MOS反相器的输入。 在一个MOS逆变器中连接一个液晶显示器,该液晶显示器指示特定范围内的直流电压是否被施加到直流电压指示器的两个端子。 振荡器电路的两个端子输入具有非常高的阻抗,并且在相当宽的直流电压范围内工作。