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1. 发明授权

US08814103B2 Position control system for cross coupled operation of fly-by-wire control columns 有权
标题翻译：线控控制柱交叉耦合运行的位置控制系统
公开(公告)号：US08814103B2
公开(公告)日：2014-08-26
申请号：US12844867
申请日：2010-07-28
申请人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
发明人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
IPC分类号： B64C13/04
CPC分类号： G05G11/00 , B64C13/12 , B64C13/503 , G05G5/03
摘要： A aircraft control system is provided that provides tactile feedback between control columns of the aircraft relating to discrepancies in the control inputs to the sticks of the respective control columns. In one implementation, the sticks each have an associated feedback assembly that is adjustable relative to mechanical ground to adjust the feedback profile applied to the corresponding stick. The position of each feedback assembly is adjusted based on a relative displacement between the other feedback assembly and its corresponding stick to provide active feedback relating to the control of the other control column.
摘要翻译：提供一种飞行器控制系统，其提供与飞机相关控制列的控制输入中的差异的飞机的控制列之间的触觉反馈。在一个实施方案中，棒各自具有相对于机械接地可调节的相关联的反馈组件，以调整施加到相应棒的反馈轮廓。基于其他反馈组件与其对应的杆之间的相对位移来调整每个反馈组件的位置，以提供与另一控制列的控制有关的主动反馈。

2. 发明申请

US20120025029A1 Position Control System for Cross Coupled Operation of Fly-By-Wire Control Columns 有权
标题翻译：电线控制柱交叉耦合位置控制系统
公开(公告)号：US20120025029A1
公开(公告)日：2012-02-02
申请号：US12844867
申请日：2010-07-28
申请人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
发明人： Zenon P. Szulyk , Ganga P. Jayaraman , Charles C. Frayman , Brian P. Dyra , Darryl S. Stachniak
IPC分类号： B64C13/12
CPC分类号： G05G11/00 , B64C13/12 , B64C13/503 , G05G5/03
摘要： A aircraft control system is provided. that provides tactile feedback between control columns of the aircraft relating to discrepancies in the control inputs to the sticks of the respective control columns. In one implementation, the sticks each have an associated feedback assembly that is adjustable relative to mechanical ground to adjust the feedback profile applied to the corresponding stick. The position of each feedback assembly is adjusted based on a relative displacement between the other feedback assembly and its corresponding stick to provide active feedback relating to the control of the other control column.
摘要翻译：提供飞机控制系统。这在飞机的控制列之间提供触觉反馈，涉及到各个控制列的支杆的控制输入中的差异。在一个实施方案中，棒各自具有相对于机械接地可调节的相关联的反馈组件，以调整施加到相应棒的反馈轮廓。基于其他反馈组件与其对应的杆之间的相对位移来调整每个反馈组件的位置，以提供与另一控制列的控制有关的主动反馈。

3. 发明授权

US08659403B2 Motor generated detent feel 有权
标题翻译：电机产生制动感
公开(公告)号：US08659403B2
公开(公告)日：2014-02-25
申请号：US13336666
申请日：2011-12-23
申请人： Charles C. Frayman
发明人： Charles C. Frayman
IPC分类号： G08B6/00
CPC分类号： B64C13/10 , Y02T50/44 , Y10T74/20396
摘要： A control stick system for simulating a detent mechanism in an aircraft is provided. The detent mechanism is simulated by a motor operably coupled to a lever and configured to bias the lever such that the user experiences the feel of a traditional detent mechanism. A controller operates the motor that provides the simulated detent by receiving data from multiple sensors regarding the position and the speed of the lever and the position and the speed of a rotor assembly of the motor. Using the position and the speed measurements, the controller is able to detect when the lever is entering a specific zone of a simulated detent range. Depending on what zone the lever is in, within the simulated detent range, the controller is configured to provide a different drive current to the motor.
摘要翻译：提供了一种用于模拟飞行器中的制动机构的控制杆系统。制动机构由可操作地联接到杠杆并被配置为偏置杠杆的马达来模拟，使得使用者体验到传统制动机构的感觉。控制器通过从多个传感器接收关于杆的位置和速度以及马达的转子组件的位置和速度的数据来操作提供模拟制动爪的马达。使用位置和速度测量，控制器能够检测杆何时进入模拟定位范围的特定区域。根据控制杆所在的区域，在模拟定位范围内，控制器配置为向电机提供不同的驱动电流。

4. 发明申请

US20130162418A1 MOTOR GENERATED DETENT FEEL 有权
标题翻译：电动发电机感应
公开(公告)号：US20130162418A1
公开(公告)日：2013-06-27
申请号：US13336666
申请日：2011-12-23
申请人： Charles C. Frayman
发明人： Charles C. Frayman
IPC分类号： B64C13/50 , G08B6/00
CPC分类号： B64C13/10 , Y02T50/44 , Y10T74/20396
摘要： A control stick system for simulating a detent mechanism in an aircraft is provided. The detent mechanism is simulated by a motor operably coupled to a lever and configured to bias the lever such that the user experiences the feel of a traditional detent mechanism. A controller operates the motor that provides the simulated detent by receiving data from multiple sensors regarding the position and the speed of the lever and the position and the speed of a rotor assembly of the motor. Using the position and the speed measurements, the controller is able to detect when the lever is entering a specific zone of a simulated detent range. Depending on what zone the lever is in, within the simulated detent range, the controller is configured to provide a different drive current to the motor.
摘要翻译：提供了一种用于模拟飞行器中的制动机构的控制杆系统。制动机构由可操作地联接到杠杆并被配置为偏置杠杆的马达来模拟，使得使用者体验到传统制动机构的感觉。控制器通过从多个传感器接收关于杆的位置和速度以及马达的转子组件的位置和速度的数据来操作提供模拟制动爪的马达。使用位置和速度测量，控制器能够检测杆何时进入模拟定位范围的特定区域。根据控制杆所在的区域，在模拟定位范围内，控制器配置为向电机提供不同的驱动电流。

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