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1. 发明授权

US06208247B1 Wireless integrated sensor network using multiple relayed communications 有权
标题翻译：无线集成传感器网络采用多中继通信
公开(公告)号：US06208247B1
公开(公告)日：2001-03-27
申请号：US09135762
申请日：1998-08-18
申请人： Jonathan R. Agre , Loren P. Clare , Henry O. Marcy, 5th , Allen J. Twarowski , William Kaiser , Wilmer A. Mickelson , Michael D. Yakos , Christian J. Loeffelholz , Jonathan R. Engdahl
发明人： Jonathan R. Agre , Loren P. Clare , Henry O. Marcy, 5th , Allen J. Twarowski , William Kaiser , Wilmer A. Mickelson , Michael D. Yakos , Christian J. Loeffelholz , Jonathan R. Engdahl
IPC分类号： G08B108
CPC分类号： G08B25/10 , G01V1/223 , G08B25/009
摘要： Wireless integrated miniature sensing stations which can be organized into a communicating network allow sensitive detection and analysis of vibration, infrared radiation, sound, or other physical signals indicative of an intruder or condition to be monitored over a wide area. The sensing stations operate on low power and include a sensor or sensors, a digital signal processor, a microprocessor, and a wireless transceiver for communication. Network communication is facilitated by multiple relayed transmissions from station to station.
摘要翻译：可以组织成通信网络的无线集成微型感测站允许敏感地检测和分析在大范围内监视入侵者或状况的振动，红外辐射，声音或其他物理信号。感测站以低功率运行，并且包括传感器或传感器，数字信号处理器，微处理器和用于通信的无线收发器。通过从站到站的多个中继传输来促进网络通信。

2. 发明授权

US07788025B2 Navigation system 有权
标题翻译：导航系统
公开(公告)号：US07788025B2
公开(公告)日：2010-08-31
申请号：US11348627
申请日：2006-02-07
申请人： Timothy V. McLaren , Wilmer A. Mickelson
发明人： Timothy V. McLaren , Wilmer A. Mickelson
IPC分类号： G01C21/12 , G01S5/02
CPC分类号： G01S19/49 , G01C21/28
摘要： A navigation system includes a first navigation module having a first operational state wherein the first navigation module does not estimate a current location and a second operational state wherein the first navigation module estimates the current location. A second navigation module performs dead reckoning in response to the first operational state of the first navigation module.
摘要翻译：导航系统包括具有第一操作状态的第一导航模块，其中第一导航模块不估计当前位置，第二导航模块还包括第一导航模块估计当前位置的第二操作状态。第二导航模块响应于第一导航模块的第一操作状态执行航位推算。

3. 发明授权

US06590524B1 Method and means for precise time synchronization 有权
标题翻译：精确时间同步的方法和手段
公开(公告)号：US06590524B1
公开(公告)日：2003-07-08
申请号：US09568104
申请日：2000-05-10
申请人： Michael G. Farley , Jeffrey J. Jorgensen , Jeffrey L. Tuohino , Susan R. Schellenberg , Wilmer A. Mickelson , Mitchell A. Corcoran
发明人： Michael G. Farley , Jeffrey J. Jorgensen , Jeffrey L. Tuohino , Susan R. Schellenberg , Wilmer A. Mickelson , Mitchell A. Corcoran
IPC分类号： G01S502
CPC分类号： G01S19/235 , G01S19/11 , G01S19/37
摘要： Disclosed is a method which synchronizes a slave time with a master time. The master time is derived from a received signal. The master time is compared to the slave time to detect any offset of the slave time relative to the master time. If an offset is detected, the slave time is adjusted to correct the offset. Also disclosed is a method of synchronizing a pseudolite transmitter time with GNSS time. The transmitter time is compared to GNSS time to detect any offset of the transmitter time. The transmitter time is adjusted to correct the offset if an offset is detected. Also disclosed is an improved pseudolite. The pseudolite has a pseudolite transmitter and GNSS receiver. The pseudolite transmitter time is synchronized with GNSS time.
摘要翻译：公开了一种使从时间与主时间同步的方法。主时间来自接收信号。将主机时间与从机时间进行比较，以检测从机时间相对于主机时间的任何偏移。如果检测到偏移，则调整从机时间以校正偏移。还公开了一种使伪卫星发射机时间与GNSS时间同步的方法。将发射机时间与GNSS时间进行比较，以检测发射机时间的任何偏移。如果检测到偏移，则调整发射机时间以校正偏移。还公开了一种改进的伪卫星。伪卫星具有伪卫星发射机和GNSS接收机。伪卫星发射机时间与GNSS时间同步。

4. 发明授权

US6163021A Navigation system for spinning projectiles 有权
标题翻译：射弹导弹系统
公开(公告)号：US6163021A
公开(公告)日：2000-12-19
申请号：US211534
申请日：1998-12-15
申请人： Wilmer A. Mickelson
发明人： Wilmer A. Mickelson
IPC分类号： F41G7/30 , G01S19/53 , F41G7/00 , F42B15/01
CPC分类号： F41G7/305
摘要： A navigation system for spinning projectiles using a magnetic spin sensor to measure the projectile roll angle by sensing changes in magnetic flux as the projectile rotates through the earth's magnetic field is disclosed. The magnetic spin sensor measurements are used to despin a body reference frame such that position, velocity, and attitude of the projectile can be determined by using a strapdown inertial navigation system (INS) algorithm. More particularly, a multisensor concept is used to measure pitch and yaw angular rates, by measuring Coriolis acceleration along the roll axis and demodulating the pitch and yaw rates therefrom.
摘要翻译：公开了一种用于使用磁性自旋传感器旋转射弹的导航系统，通过在射弹旋转穿过地球磁场时感测磁通量的变化来测量射弹侧倾角。使用磁自旋传感器测量来解析身体参考系，使得可以使用捷联惯导系统（INS）算法来确定射弹的位置，速度和姿态。更具体地，多传感器概念用于通过测量沿轴线的科里奥利加速度并且从其中解调俯仰和偏航速率来测量俯仰角和偏航角速率。

5. 发明授权

US6031487A GPS pseudolite and receiver system using high anti-jam pseudolite signal structure 失效
标题翻译： GPS伪卫星和接收系统采用高抗伪伪信号结构
公开(公告)号：US6031487A
公开(公告)日：2000-02-29
申请号：US47566
申请日：1998-03-25
申请人： Wilmer A. Mickelson
发明人： Wilmer A. Mickelson
IPC分类号： G01S5/14 , G01S19/04 , G01S19/10 , G01S19/44 , G01S19/46 , G01S5/02 , H04B7/185
CPC分类号： G01S19/11 , G01S19/215 , G01S19/256 , G01S19/258 , G01S19/37
摘要： Disclosed is a GPS pseudolite transmitter, receiver and navigation system. The GPS pseudolite transmitter is adapted to transmit a first phase modulated L-band signal at a first signal pulse repetition rate having an associated first period time duration. The first phase modulated L-band signal is modulated with a short period code having a code epoch of at least about one millisecond. For each consecutive transmission pulse having the first period time duration, the pseudolite transmitter transmits the first phase modulated L-band signal during less than one half of the first period time duration, and for at least about 1 millisecond so that the first pseudolite transmitter transmits an epoch of the short period code during each transmission pulse. A receiver is adapted to receive the first phase modulated L-band signal from the first pseudolite transmitter, at times when it is not integrating phase modulated L-band signals from other GPS pseudolites transmitters, such that cross-correlation with other phase modulated L-band signals is minimized. Furthermore, the receiver is adapted to receive the L-band satellite signal during intervals when no pseudolite signals are being received.
摘要翻译：公开了一种GPS伪卫星发射机，接收机和导航系统。 GPS伪卫星发射机适于以具有相关联的第一周期持续时间的第一信号脉冲重复率发射第一相位调制的L波段信号。第一相位调制的L波段信号用具有至少约一毫秒的码时代的短周期码进行调制。对于具有第一周期持续时间的每个连续传输脉冲，伪卫星发射机在小于第一周期持续时间的一半的时间内发射第一相位调制的L波段信号，并且至少约1毫秒，使得第一伪卫星发射机发送在每个传输脉冲期间短周期代码的时代。接收机适于从第一伪卫星发射机接收第一相位调制的L波段信号，这时它不是来自其他GPS伪卫星发射机的相位调制的L波段信号的积分，使得与其它相位调制的L波段信号的互相关，频带信号被最小化。此外，接收机适于在不接收伪卫星信号的间隔期间接收L波段卫星信号。

6. 发明授权

US5917448A Attitude determination system with sequencing antenna inputs 失效
标题翻译：具有测序天线输入的姿态确定系统
公开(公告)号：US5917448A
公开(公告)日：1999-06-29
申请号：US908418
申请日：1997-08-07
申请人： Wilmer A. Mickelson
发明人： Wilmer A. Mickelson
IPC分类号： G01S19/21 , G01S5/02 , G01S19/26
CPC分类号： G01S19/53 , G01S19/36
摘要： An attitude determination system uses multiple antenna inputs which are time-multiplexed into a multi-channel receiver. Each channel tracks one incoming signal from a known or ascertainable source. For each of the incoming signals being tracked, digital processing can be used to determine range differences between the different antenna elements for that incoming signal, and to compute attitude based on the range differences and the known configuration of the attenna elements relative to each other.
摘要翻译：姿态确定系统使用时间多路复用到多声道接收机中的多个天线输入。每个通道跟踪来自已知或可确定源的一个输入信号。对于被跟踪的每个输入信号，数字处理可用于确定用于该输入信号的不同天线元件之间的范围差异，并且基于相对于彼此的天线元件的距离差和已知配置来计算姿态。

7. 发明授权

US4574245A Multisensor demodulator and A/D converter 失效
标题翻译：多传感器解调器和A / D转换器
公开(公告)号：US4574245A
公开(公告)日：1986-03-04
申请号：US432874
申请日：1982-10-05
申请人： Wilmer A. Mickelson
发明人： Wilmer A. Mickelson
IPC分类号： G01P15/08 , H03D3/00 , G01P9/02
CPC分类号： G01P15/08
摘要： An apparatus and technique is disclosed for demodulating an FM signal provided as an output from a sensor assembly. The FM signal may represent acceleration as measured by a sensor included on a rotating wheel in an attitude and heading reference system. The FM signal is demodulated and directly converted to a digital value to provide digital signal processing with improved performance characteristics. The demodulation is accomplished by detecting each FM cycle to provide a signal output at the occurrence of each cycle. A reference mark on the rotating wheel is detected for providing synchronization such that a demodulation angle of the rotating wheel can be determined. The demodulation angle is represented as a sine value which is read for each FM cycle during one sensor revolution and summed with all previous sine values detected during that one revolution. A digital output of that sum is then provided as a measurement of acceleration or other parameter along an axis of the system.
摘要翻译：公开了用于解调作为传感器组件的输出提供的FM信号的装置和技术。 FM信号可以表示由包括在姿态和航向参考系统中的旋转轮上的传感器测量的加速度。 FM信号被解调并直接转换为数字值，以提供具有改进的性能特征的数字信号处理。通过检测每个FM周期以在每个周期发生时提供信号输出来完成解调。检测旋转轮上的参考标记以提供同步，使得可以确定旋转轮的解调角度。解调角度被表示为在一个传感器旋转期间为每个FM循环读取的正弦值，并与在该一转期间检测到的所有先前正弦值相加。然后将该和的数字输出作为沿着系统的轴的加速度或其它参数的测量值提供。

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