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公开(公告)号：US08410412B2
公开(公告)日：2013-04-02
申请号：US13226749
申请日：2011-09-07
申请人： Chris E. Geswender , Stevie Alejandro , Paul Vesty
发明人： Chris E. Geswender , Stevie Alejandro , Paul Vesty
摘要： A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile using aerodynamic forces. Aerodynamic surfaces, such as lift-producing surfaces, for example tails or canards, are coupled to the collar, and rotate with the collar. An actuator system or mechanism controls orienting of the lift-producing surfaces, such as tilting of the lift producing surfaces, to direct the collar into a desired position relative to a longitudinal axis of the projectile, and to maintain the collar in that position. With such a control the projectile is able to be steered using bank-to-turn maneuvering. The actuator system may use any of a variety of mechanisms to move the lift-producing surfaces, thereby positioning the collar.
摘要翻译： 具有以其轴线旋转的旋转或滚动机身的抛射体，机动车辆或潜水艇具有可以使用空气动力力相对于射弹的纵向轴线定位的轴环。 空气动力学表面，例如提升产生表面，例如尾部或者尾部，联接到套环上，并与套环一起旋转。 致动器系统或机构控制提升产生表面的定向，例如提升产生表面的倾斜，以将轴环引导到相对于抛射体的纵向轴线的期望位置，并将轴环保持在该位置。 有了这样的控制，射弹能够使用银行对转机动来引导。 致动器系统可以使用各种机构中的任一种来移动提升产生表面，从而定位套环。
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公开(公告)号：US20120175459A1
公开(公告)日：2012-07-12
申请号：US13226749
申请日：2011-09-07
申请人： Chris E. Geswender , Stevie Alejandro , Paul Vesty
发明人： Chris E. Geswender , Stevie Alejandro , Paul Vesty
摘要： A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile using aerodynamic forces. Aerodynamic surfaces, such as lift-producing surfaces, for example tails or canards, are coupled to the collar, and rotate with the collar. An actuator system or mechanism controls orienting of the lift-producing surfaces, such as tilting of the lift producing surfaces, to direct the collar into a desired position relative to a longitudinal axis of the projectile, and to maintain the collar in that position. With such a control the projectile is able to be steered using bank-to-turn maneuvering. The actuator system may use any of a variety of mechanisms to move the lift-producing surfaces, thereby positioning the collar.
摘要翻译： 具有以其轴线旋转的旋转或滚动机身的抛射体，机动车辆或潜水艇具有可以使用空气动力力相对于射弹的纵向轴线定位的轴环。 空气动力学表面，例如提升产生表面，例如尾部或者尾部，联接到套环上，并与套环一起旋转。 致动器系统或机构控制提升产生表面的定向，例如提升产生表面的倾斜，以将轴环引导到相对于抛射体的纵向轴线的期望位置，并将轴环保持在该位置。 有了这样的控制，射弹能够使用银行对转机动来引导。 致动器系统可以使用各种机构中的任一种来移动提升产生表面，从而定位套环。
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公开(公告)号：US20100133374A1
公开(公告)日：2010-06-03
申请号：US12325352
申请日：2008-12-01
IPC分类号： F42B15/01
摘要： A projectile, such as a missile, rolls during at least a portion of its flight, while retaining its roll reference to enable navigation during the rolling period of flight. The roll reference may be retained by using a sensor, such as magnetometer, to periodically check and correct the roll reference. Alternatively or in addition the missile may alternate roll directions, for example varying roll rate in a substantially sinusoidal function. By rolling the missile inaccuracies in an inertial measurement unit (IMU) of the missile may be ameliorated by being to a large extent canceled out by the changes in orientation of the missile as the missile rolls. This enables use of IMUs with lower accuracy than would otherwise be required to obtain accurate flight. Thus accurate flight may be accomplished with less costly IMUs, without sacrificing the ability to navigate.
摘要翻译： 飞弹，如导弹，在其飞行的至少一部分内滚动，同时保留其滚动参考，以便在飞行的滚动期间启用导航。 可以通过使用诸如磁力计的传感器来保持辊参考，以周期性地检查和校正辊参考。 或者或另外，导弹可以交替滚动方向，例如在基本正弦函数中改变滚动速率。 通过在导弹的惯性测量单位（IMU）中滚动导弹不准确度，可以在很大程度上被导弹导弹导弹方向的变化所抵消。 这使得能够使用比获得准确飞行所需的准确度更低的IMU。 因此，可以用较便宜的IMU来实现准确的飞行，而不会牺牲导航能力。
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公开(公告)号：US08993948B2
公开(公告)日：2015-03-31
申请号：US13215497
申请日：2011-08-23
摘要： A spinning, rolling, or roll-stabilized vehicle, such as a projectile, includes a fuselage that rotates about its longitudinal axis (spins) during flight. A collar is positionable relative to the fuselage to steer the projectile, with the collar having ailerons to provide a roll force to position the collar. The collar also has elevators to provide lateral force to steer the projectile. The positioning of the collar may be accomplished by moderating the roll force of the ailerons to hold the position of the collar substantially constant with regard to a longitudinal axis of the projectile. The ailerons passively change angle of attack with changes in the dynamic pressure of the projectile. At low speeds the ailerons have a relatively large angle of attack, and at high speeds, the ailerons resiliently reduce their angles of attack, avoiding large rolling forces on the collar.
摘要翻译： 旋转，滚动或滚动稳定的车辆，如射弹，包括在飞行期间围绕其纵向轴线（旋转）旋转的机身。 一个衣领可相对于机身定位以引导抛射体，其中衣领具有副翼以提供滚动力来定位套环。 领子还有电梯提供侧向力来引导射弹。 套环的定位可以通过调节副翼的滚动力来实现，以便相对于射弹的纵向轴线保持轴环的位置基本恒定。 副翼被动地改变了射弹动态压力的变化。 在低速时，副翼具有相对较大的迎角，而且在高速时，副翼弹性地降低了它们的迎角，避免了轴环上的大的滚动力。
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公开(公告)号：US20140312162A1
公开(公告)日：2014-10-23
申请号：US13215497
申请日：2011-08-23
IPC分类号： F42B10/64
摘要： A spinning, rolling, or roll-stabilized vehicle, such as a projectile, includes a fuselage that rotates about its longitudinal axis (spins) during flight. A collar is positionable relative to the fuselage to steer the projectile, with the collar having ailerons to provide a roll force to position the collar. The collar also has elevators to provide lateral force to steer the projectile. The positioning of the collar may be accomplished by moderating the roll force of the ailerons to hold the position of the collar substantially constant with regard to a longitudinal axis of the projectile. The ailerons passively change angle of attack with changes in the dynamic pressure of the projectile. At low speeds the ailerons have a relatively large angle of attack, and at high speeds, the ailerons resiliently reduce their angles of attack, avoiding large rolling forces on the collar.
摘要翻译： 旋转，滚动或滚动稳定的车辆，如射弹，包括在飞行期间围绕其纵向轴线（旋转）旋转的机身。 一个衣领可相对于机身定位以引导抛射体，其中衣领具有副翼以提供滚动力来定位套环。 领子还有电梯提供侧向力来引导射弹。 套环的定位可以通过调节副翼的滚动力来实现，以便相对于射弹的纵向轴线保持轴环的位置基本恒定。 副翼被动地改变了射弹动态压力的变化。 在低速时，副翼具有相对较大的迎角，而且在高速时，副翼弹性地降低了它们的迎角，避免了轴环上的大的滚动力。
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公开(公告)号：US08519313B2
公开(公告)日：2013-08-27
申请号：US12325352
申请日：2008-12-01
摘要： A projectile, such as a missile, rolls during at least a portion of its flight, while retaining its roll reference to enable navigation during the rolling period of flight. The roll reference may be retained by using a sensor, such as magnetometer, to periodically check and correct the roll reference. Alternatively or in addition the missile may alternate roll directions, for example varying roll rate in a substantially sinusoidal function. By rolling the missile inaccuracies in an inertial measurement unit (IMU) of the missile may be ameliorated by being to a large extent canceled out by the changes in orientation of the missile as the missile rolls. This enables use of IMUs with lower accuracy than would otherwise be required to obtain accurate flight. Thus accurate flight may be accomplished with less costly IMUs, without sacrificing the ability to navigate.
摘要翻译： 飞弹，如导弹，在其飞行的至少一部分内滚动，同时保留其滚动参考，以便在飞行的滚动期间启用导航。 可以通过使用诸如磁力计的传感器来保持辊参考，以周期性地检查和校正辊参考。 或者或另外，导弹可以交替滚动方向，例如在基本正弦函数中改变滚动速率。 通过在导弹的惯性测量单位（IMU）中滚动导弹不准确度，可以在很大程度上被导弹导弹导弹方向的变化所抵消。 这使得使用的IMU的比原本需要获得准确的航班精度较低。 因此，可以用较便宜的IMU来实现准确的飞行，而不会牺牲导航能力。
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公开(公告)号：US08704699B2
公开(公告)日：2014-04-22
申请号：US10706665
申请日：2003-11-12
申请人： Chris E. Geswender
发明人： Chris E. Geswender
IPC分类号： H01Q15/00
摘要： A dipole based decoy system provides an inexpensive alternative to chaff. A non-conductive filament patterned with lengths of conductive material that form dipole antennas at one or more radar frequencies is stored on the air vehicle and attached to a projectile. In response to a RWR warning, a programmed time or location or a time-to-target, a mechanism releases the projectile(s) to deploy the filament with its dipole antennas at a speed greater than or equal to the speed of the air vehicle to present an extended target or a separate false target to enemy radar. The projectile is either towed behind the air vehicle or launched away from the air vehicle. Either approach is effective to overcome Doppler and moving range gating by presenting coherent signal returns and ranges and velocities consistent with the air vehicle during a threat interval posed by the radar defense systems.
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公开(公告)号：US20140009319A1
公开(公告)日：2014-01-09
申请号：US10706665
申请日：2003-11-12
申请人： Chris E. Geswender
发明人： Chris E. Geswender
摘要： A dipole based decoy system provides an inexpensive alternative to chaff. A non-conductive filament patterned with lengths of conductive material that form dipole antennas at one or more radar frequencies is stored on the air vehicle and attached to a projectile. In response to a RWR warning, a programmed time or location or a time-to-target, a mechanism releases the projectile(s) to deploy the filament with its dipole antennas at a speed greater than or equal to the speed of the air vehicle to present an extended target or a separate false target to enemy radar. The projectile is either towed behind the air vehicle or launched away from the air vehicle. Either approach is effective to overcome Doppler and moving range gating by presenting coherent signal returns and ranges and velocities consistent with the air vehicle during a threat interval posed by the radar defense systems.
摘要翻译： 基于偶极子的诱饵系统提供了廉价的谷壳替代品。 在一个或多个雷达频率上形成偶极天线的导电材料长度图案化的非导电细丝被存储在飞行器上并附着到抛射体上。 响应于RWR警告，编程的时间或位置或时间到目标，机构释放射弹以其偶极子天线部署灯丝，速度大于或等于机动车辆的速度 向敌方雷达提出扩展目标或单独的虚假目标。 抛射体被拖在机动车辆后面或从空中车辆上离开。 任何一种方法都有效地通过在雷达防御系统构成的威胁间隔期间呈现与航空器一致的相干信号返回和范围和速度来克服多普勒和移动范围门控。
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公开(公告)号：US08344304B2
公开(公告)日：2013-01-01
申请号：US12964798
申请日：2010-12-10
申请人： Chris E. Geswender
发明人： Chris E. Geswender
摘要： Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.
摘要翻译： 用于传送导弹的方法和装置可以与包括外部皮肤的导弹一起操作。 导弹可以配置在关闭位置和打开位置。 在打开位置时，在外皮中开孔，例如将空气供给到空气呼吸引擎。 在关闭位置，孔关闭。
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公开(公告)号：US20120175458A1
公开(公告)日：2012-07-12
申请号：US13005175
申请日：2011-01-12
申请人： Chris E. Geswender
发明人： Chris E. Geswender
摘要： A projectile, air vehicle or submersible craft with a spinning or rolling fuselage, rotating on its axis, has a collar which can be positioned relative to a longitudinal axis of the projectile using aerodynamic forces. Aerodynamic surfaces, such as lift-producing surfaces, for example tails or canards, are coupled to the collar, and rotate with the collar. An actuator system or mechanism controls orienting of the lift-producing surfaces, such as tilting of the lift producing surfaces, to direct the collar into a desired position relative to a longitudinal axis of the projectile, and to maintain the collar in that position. With such a control the projectile is able to be steered using bank-to-turn maneuvering. The actuator system may use any of a variety of mechanisms to move the lift-producing surfaces, thereby positioning the collar.
摘要翻译： 具有以其轴线旋转的旋转或滚动机身的抛射体，机动车辆或潜水艇具有可以使用空气动力力相对于射弹的纵向轴线定位的轴环。 空气动力学表面，例如提升产生表面，例如尾部或者尾部，联接到套环上，并与套环一起旋转。 致动器系统或机构控制提升产生表面的定向，例如提升产生表面的倾斜，以将轴环引导到相对于抛射体的纵向轴线的期望位置，并将轴环保持在该位置。 有了这样的控制，射弹能够使用银行对转机动来引导。 致动器系统可以使用各种机构中的任一种来移动提升产生表面，从而定位套环。
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