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    • 2. 发明授权
    • Active remote sensing using a simultaneous spectral sampling technique
    • 使用同时光谱采样技术的主动遥感
    • US07009170B2
    • 2006-03-07
    • US10603695
    • 2003-06-26
    • Michael E. DobbsJeff D. PruittMatthew L. GypsonBenjamin R. Neff
    • Michael E. DobbsJeff D. PruittMatthew L. GypsonBenjamin R. Neff
    • H01J40/14H01J5/16
    • G01N21/39G01N21/3151G01N33/004G01N2021/1793G01N2021/396G01N2201/067G01N2201/0691
    • A system for sensing a characteristic of a sample may include a tunable source configured to emit optical radiation that varies over a wavelength range at a sweep frequency and a reference source configured to emit optical radiation at a reference wavelength. A first modulator may be configured to modulate the first optical radiation at a first frequency, and a second modulator may be configured to modulate the second optical radiation at a second frequency that is different from the first frequency and the sweep frequency. A science detector may be configured to detect the optical radiation from the first modulator and the second modulator after interaction with the sample and generate a science signal. A number of lock-in amplifiers may be respectively configured to generate components of the science signal that are present at the first and second frequencies. A processor may be configured to determine a characteristic of the sample based on the components of the science signal that are present at the first and second frequencies.
    • 用于感测样本特征的系统可以包括被配置为发射在扫描频率处的波长范围内变化的光辐射的可调谐源和被配置为发射参考波长的光辐射的参考源。 第一调制器可以被配置为以第一频率调制第一光辐射,并且第二调制器可以被配置为以不同于第一频率和扫频的第二频率来调制第二光辐射。 科学检测器可以被配置为在与样本相互作用之后检测来自第一调制器和第二调制器的光辐射并产生科学信号。 多个锁定放大器可以分别被配置为产生存在于第一和第二频率的科学信号的分量。 处理器可以被配置为基于在第一和第二频率处存在的科学信号的分量来确定样本的特性。
    • 8. 发明授权
    • Spacecraft payload exchange system
    • 航天器有效载荷交换系统
    • US5429328A
    • 1995-07-04
    • US977075
    • 1992-11-16
    • Michael E. DobbsDonald B. Jones
    • Michael E. DobbsDonald B. Jones
    • B64G1/64
    • B64G1/646B64G1/641
    • A method of manufacturing in space and a spacecraft assembly to accomplish such manufacture. The spacecraft assembly includes a spacecraft including a plurality of canister compartments circumferentially spaced about the central axis of the spacecraft and opening in a docking face of the spacecraft, a plurality of canisters respectively positioned in the compartments, and a passive docking mechanism proximate the docking face and proximate the central axis, and a service vehicle comprising a plurality of canister compartments spaced circumferentially about the central axis of the service vehicle, a plurality of canisters respectively positioned in the compartments, and a manipulator assembly including an active docking structure, including a boom extending forwardly from the docking face, and a canister handling assembly mounted on the boom. In one embodiment, the spacecraft remains permanently in orbit, a manufacturing process is performed on the spacecraft to produce an end product which is housed in the canisters, and the service vehicle periodically visits the orbiting spacecraft to perform a canister exchange with the spacecraft, utilizing the canister exchange with the spacecraft, utilizing the canister handling assembly, and replenishing the spacecraft supplies.
    • 空间制造方法和航天器组件来实现这种制造。 航天器组件包括航天器,其包括围绕航天器的中心轴线周向隔开并在飞船的对接面上开口的多个罐隔室,分别定位在舱室中的多个罐和靠近对接面的被动对接机构 并且靠近中心轴线,以及服务车辆,其包括围绕服务车辆的中心轴线周向间隔开的多个罐室,分别定位在隔间中的多个罐,以及包括主动对接结构的操纵器组件,包括吊杆 从对接面向前延伸,以及安装在起重臂上的罐处理组件。 在一个实施例中,航天器永久地保持在轨道上,对航天器执行制造过程以产生容纳在罐中的最终产品,并且服务车辆周期性地访问轨道航天器以与飞船进行罐交换,利用 罐与飞船交换,利用罐处理组件,并补充航天器耗材。
    • 9. 发明授权
    • Active remote sensing using lock-in amplifiers and beam steering
    • 使用锁定放大器和波束转向的主动遥感
    • US07009705B1
    • 2006-03-07
    • US10197247
    • 2002-07-18
    • Michael E. DobbsAllan Roberts
    • Michael E. DobbsAllan Roberts
    • G01N21/55
    • G01S17/87G01S7/497G01S17/32G01S17/89
    • A remote sensing platform for sensing a target may include a source configured to emit optical radiation toward the target. A device may be configured to dither the emitted optical radiation to alternately illuminate a number of locations on the target. A first detector may be configured to detect radiation reflected from a first location of the number of locations and to generate a first signal. A first lock-in amplifier may be configured to process the first signal. A second detector may be configured to detect radiation reflected from a second location of the number of locations and to generate a second signal. A second lock-in amplifier may be configured to process the second signal.
    • 用于感测目标的遥感平台可以包括被配置为朝向目标发射光辐射的源。 设备可以被配置为使所发射的光辐射抖动以交替地照射目标上的多个位置。 第一检测器可以被配置为检测从位置的数量的第一位置反射的辐射并且产生第一信号。 第一锁定放大器可以被配置为处理第一信号。 第二检测器可以被配置为检测从位置的数量的第二位置反射的辐射并且产生第二信号。 第二锁定放大器可以被配置为处理第二信号。