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1. 发明授权

US08179598B1 Scanning wide field telescope (SWIFT) spaceflight-deployed payload 有权
标题翻译：扫描宽视场望远镜（SWIFT）空间部署的有效载荷
公开(公告)号：US08179598B1
公开(公告)日：2012-05-15
申请号：US12541110
申请日：2009-08-13
申请人： David Stubbs , Alan Duncan , Kenneth R. Lorell , Howard C. Holmes
发明人： David Stubbs , Alan Duncan , Kenneth R. Lorell , Howard C. Holmes
IPC分类号： G02B23/08 , G02B23/00
CPC分类号： G02B7/183 , G02B23/06
摘要： A telescope comprises a folding reflector comprising a plurality of sections configured to fold at a plurality of substantially parallel hinges, a support structure configured to support at least two of the plurality of sections of the folding reflector and further configured to fold at one of the plurality of substantially parallel hinges, a corrector assembly configured to deploy from a stowed position in which an optical axis of the corrector assembly is substantially parallel to the parallel hinges to a deployed position in which the optical axis is substantially perpendicular to the folding reflector when the folding reflector is deployed. The telescope further comprises a hexapod configured to stow and deploy the corrector assembly.
摘要翻译：望远镜包括折叠反射器，该折叠反射器包括构造成在多个基本上平行的铰链处折叠的多个部分;支撑结构，其构造成支撑折叠反射器的多个部分中的至少两个部分，并进一步构造成在多个部分之一处折叠基本上平行的铰链，校正器组件，构造成从收起位置展开，其中校正器组件的光轴基本上平行于平行铰链到展开位置，在展开位置，当折叠的折叠反射器反射器被部署。望远镜还包括配置成收起和展开校正器组件的六足体。

2. 发明授权

US5245830A Adaptive error correction control system for optimizing stirling refrigerator operation 失效
标题翻译：自适应纠错控制系统，用于优化冰箱操作
公开(公告)号：US5245830A
公开(公告)日：1993-09-21
申请号：US892855
申请日：1992-06-03
申请人： Jean-Noel Aubrun , Kenneth R. Lorell , Paul J. Reshatoff , Robert R. Clappier
发明人： Jean-Noel Aubrun , Kenneth R. Lorell , Paul J. Reshatoff , Robert R. Clappier
IPC分类号： F25B9/14 , G05B5/01 , G05B21/02
CPC分类号： G05B21/02 , F25B9/14 , G05B5/01 , F25B2309/001 , F25B2500/13
摘要： An adaptive control includes a digital error correction system (DECS) to reduce control system error to near zero by anticipating a problem and feeding forward in time a correction to deal with the problem before it happens. The adaptive control is used in a controlled system of the kind which is cyclical in operation and which operates in response to repetitive cycle commands so that the operation of the system is substantially predictable for a significant number of cycles of operation. The adaptive control is incorporated in a refrigerator system in which two Stirling cycle refrigerators are mounted in opposition to one another. The adaptive control permits accurate control of the command waveform frequency and shape, enables the refrigerator system to be more thermodynamically efficient, and enables the two refrigerators to exactly cancel each other's vibration.
摘要翻译：一种自适应控制包括一个数字纠错系统（DECS），通过预测问题，将控制系统误差减少到接近于零，并且在发生之前及时向前馈送纠正处理该问题。自适应控制被用于在操作中是周期性的并且响应于重复循环命令而操作的受控系统，使得系统的操作对于大量的操作循环是可以预见的。自适应控制被并入冰箱系统中，其中两个斯特林循环冰箱彼此相对安装。自适应控制允许对指令波形频率和形状的精确控制，使得冰箱系统更具有热力学效能，并且使两个冰箱能够精确地抵消彼此的振动。

3. 发明授权

US07380950B1 Hybrid high-bandwidth deformable fast steering mirror 失效
标题翻译：混合高带宽可变形快速转向镜
公开(公告)号：US07380950B1
公开(公告)日：2008-06-03
申请号：US11057199
申请日：2005-02-15
申请人： Kenneth R. Lorell , Stephen R. Winzer , Craig L. Horn , Natarajan Shankar , Robert R. Clappier
发明人： Kenneth R. Lorell , Stephen R. Winzer , Craig L. Horn , Natarajan Shankar , Robert R. Clappier
IPC分类号： G02B5/08
CPC分类号： G02B26/0825
摘要： A high-bandwidth deformable fast steering mirror (“HDFSM”) system, including an electromechanical fast steering mirror (“FSM”) apparatus, and a deformable mirror (“DM”) apparatus mounted on the electromechanical FSM apparatus. The DM apparatus further includes a DM substrate, a backplane assembly, a plurality of electrostrictive actuators in physical communication with and between the DM substrate and the backplane assembly, for deforming the DM substrate, and a plurality of strain gauges, each strain gauge mounted on one of the plurality of electrostrictive actuators, the plurality of strain gauges measuring individual positions of the plurality of electrostrictive actuators and transmitting the positions as actuator position signals. The high-bandwidth deformable FSM also includes a closed-loop control system, the control system controlling the electromechanical FSM apparatus and the DM apparatus based upon a command input and the actuator position signals.
摘要翻译：一种高带宽可变形快速转向镜（“HDFSM”）系统，包括安装在机电式FSM装置上的机电快速转向镜（“FSM”）装置和可变形反射镜（“DM”）装置。 DM设备还包括DM基板，背板组件，与DM基板和背板组件物理连通并且在DM基板和背板组件之间的多个电致伸缩致动器，用于使DM基板变形，以及多个应变计，每个应变计安装在多个电致伸缩致动器中的一个，多个应变计测量多个电致伸缩致动器的各个位置，并将位置作为致动器位置信号传输。高带宽可变形FSM还包括闭环控制系统，控制系统基于命令输入和执行器位置信号控制机电FSM装置和DM装置。

4. 发明授权

US4012018A All sky pointing attitude control system 失效
标题翻译：全天空指向姿态控制系统
公开(公告)号：US4012018A
公开(公告)日：1977-03-15
申请号：US403695
申请日：1973-10-04
申请人： Kenneth R. Lorell , James P. Murphy
发明人： Kenneth R. Lorell , James P. Murphy
IPC分类号： B64G1/24 , B64G1/28 , B64G1/36 , B64G1/10
CPC分类号： B64G1/24 , B64G1/288 , B64G1/361 , B64G1/363
摘要： In a strapped-down gyroscope space vehicle attitude control system, a method and apparatus are provided for gyro drift and input axis misalignment error compensation employing a sun and a star tracker and preselected vehicle calibration maneuvers. During the preselected maneuvers using the sun and a star as external references, the outputs of two-axis strapped-down gyroscopes nominally aligned with the optical axis of the sun and star trackers are measured. The measured outputs provide gyro drift calibration, roll, pitch and yaw axis scale factors and values corresponding to the degree of nonorthogonality between the roll axis and the pitch and yaw gyro input axes and the nonorthogonality of the roll and pitch axes relative to the yaw axis. With the calibration data so obtained stored in a special purpose digital computer, the vehicle is then rolled and yawed through precomputed angles as modified by the calibration data to acquire a target without further recourse to external references.
摘要翻译：在捆扎式陀螺仪空间车辆姿态控制系统中，提供了一种使用太阳和星形跟踪器的陀螺漂移和输入轴未对准误差补偿的方法和装置以及预选车辆校准操作。在使用太阳和星形作为外部参考的预选演习期间，测量名义上与太阳和星形跟踪器的光轴对准的双轴捆绑式陀螺仪的输出。测量的输出提供陀螺仪漂移校准，滚动，俯仰和偏航轴比例因子和对应于滚动轴与俯仰和偏航陀螺仪输入轴之间的非正交性程度以及相对于偏转轴的滚动和俯仰轴的非正交性的值。使用如此获得的校准数据存储在专用数字计算机中，然后通过由校准数据修改的预计算角度来滚动和偏航，以获得目标而不需要进一步追求外部参考。

5. 发明授权

US07275285B1 Deployment hinge 有权
标题翻译：部署铰链
公开(公告)号：US07275285B1
公开(公告)日：2007-10-02
申请号：US10986881
申请日：2004-11-15
申请人： Kenneth R. Lorell , Patrick J. Champagne
发明人： Kenneth R. Lorell , Patrick J. Champagne
IPC分类号： E05D11/10
CPC分类号： B64G1/222 , Y10T16/5381 , Y10T16/5383 , Y10T16/5402
摘要： A deployment hinge for deploying an appendage, including a movable portion affixed to the appendage, and a stationary portion affixed to a stationary body. In a non-deployed state, the movable portion is mechanically engaged with the stationary portion and a mechanical load is transferred between the stationary portion and the movable portion. In a deployed state, the movable portion is mechanically disengaged from the stationary portion, and a mechanical load is prevented from being transferred to the movable portion from the stationary portion.
摘要翻译：用于展开附件的展开铰链，包括固定在附属物上的活动部分和固定在固定体上的固定部分。在非展开状态下，可移动部分与固定部分机械接合，并且机械负载在固定部分和可移动部分之间传递。在展开状态下，可移动部分与固定部分机械地脱开，并且防止机械负载从静止部分转移到可动部分。

6. 发明授权

US07086300B1 Large stroke linear motion flexural apparatus 有权
标题翻译：大行程直线运动弯曲装置
公开(公告)号：US07086300B1
公开(公告)日：2006-08-08
申请号：US10412565
申请日：2003-04-11
申请人： Donald F. Zacharie , Kenneth R. Lorell , Jean-Noel Auburn
发明人： Donald F. Zacharie , Kenneth R. Lorell , Jean-Noel Auburn
IPC分类号： F16H61/06
CPC分类号： F16F15/073 , F16F1/027 , F16F2230/0052 , F16F2230/34 , F16H21/04
摘要： Embodiments of the present invention are directed to a linear motion flexural apparatus to provide friction-free linear travel for large stroke motion. In one embodiment, a linear motion flexural apparatus comprises a first member having a first surface, and a second member having a second surface which is spaced from the first surface of the first member. One of the first member and the second member is movable relative to another one of the first member and the second member in a linear direction. At least one sheet is disposed between the first surface of the first member and the second surface of the second member. Each sheet has a first edge portion and a second edge portion generally opposite from the first edge portion. The first edge portion is attached to the first surface of the first member. The second edge portion is attached to the second surface of the second member. Each sheet has a curved portion with a shape which is substantially unchanged during movement between the first member and the second member in the linear direction.
摘要翻译：本发明的实施例涉及一种用于为大行程运动提供无摩擦线性行程的直线运动弯曲装置。在一个实施例中，线性运动弯曲装置包括具有第一表面的第一构件和具有与第一构件的第一表面间隔开的第二表面的第二构件。第一构件和第二构件中的一个可相对于第一构件和第二构件中的另一个在线性方向上移动。至少一个片材设置在第一构件的第一表面和第二构件的第二表面之间。每个片材具有大致与第一边缘部分相反的第一边缘部分和第二边缘部分。第一边缘部分附接到第一构件的第一表面。第二边缘部分附接到第二构件的第二表面。每个片材具有弯曲部分，其形状在第一构件和第二构件之间在线性方向上移动期间基本上不变。

7. 发明授权

US5359520A Adaptive error correction control system for optimizing mirror positioning in a spatial chopping or scanning telescope 失效
标题翻译：自适应纠错控制系统，用于优化空间斩波或扫描望远镜中的镜像定位
公开(公告)号：US5359520A
公开(公告)日：1994-10-25
申请号：US895313
申请日：1992-06-08
申请人： Jean-Noel Aubrun , Kenneth R. Lorell , Paul J. Reshatoff
发明人： Jean-Noel Aubrun , Kenneth R. Lorell , Paul J. Reshatoff
IPC分类号： F25B9/14 , G05B5/01 , G05B21/02 , G05B13/02 , G05B19/18 , G05B5/10
CPC分类号： G05B21/02 , F25B9/14 , G05B5/01 , F25B2309/001 , F25B2500/13
摘要： An adaptive control includes a digital error correction system (DECS) to reduce control system error to near zero by anticipating a problem and feeding forward in time a correction to deal with the problem before it happens. The adaptive control is used in a controlled system of the kind which is cyclical in operation and which operates in response to repetitive cycle commands so that the operation of the system is substantially predictable for a significant number of cycles of operation. The adaptive control is incorporated in a spatial chopping or scanning telescope system of the kind in which a telescope mirror is moved in repetitive cycle motions and in a rigidly prescribed pattern between varied orientations and wherein the mirror is held for a prescribed, relatively long period of time in each orientation and is moved rapidly in a relatively short period of time from one orientation to another. The adaptive control permits accurate control of the command waveform frequency and shape, enables the telescope system to keep position error near zero by using, in combination with the feedback loop, a feed forward loop directly driving the actuators during the transition period and actively holding the mirror in position during the dwell periods. The adaptive control provides the ability to eliminate overshoot and ringing, because the force command provides the precise amount of braking required to exactly stop the mirror motion.
摘要翻译：一种自适应控制包括一个数字纠错系统（DECS），通过预测问题，将控制系统误差减少到接近于零，并且在发生之前及时向前馈送纠正处理该问题。自适应控制被用于在操作中是周期性的并且响应于重复循环命令而操作的受控系统，使得系统的操作对于大量的操作循环是可以预见的。自适应控制被结合在这样的空间斩波或扫描望远镜系统中，其中望远镜在重复循环运动中以刚性规定的方式移动，并且其中镜子保持规定的较长时间段时间在每个方向，并在相对较短的时间段内从一个方向快速移动到另一个方向。自适应控制允许对指令波形频率和形状的精确控制，使望远镜系统能够通过与反馈回路结合使用在过渡期间直接驱动致动器的前馈回路来保持位置误差接近于零，并且主动地保持镜像在停留期间的位置。自适应控制提供消除过冲和振铃的能力，因为力指令提供准确停止镜面运动所需的精确量的制动。

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