公开(公告)号：US08214089B2

公开(公告)日：2012-07-03

申请号：US12942534

申请日：2010-11-09

申请人： Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Alvaro Vito Polati de Souza ,  Eduardo da Silva Martins ,  Marco Tulio Sguerra Vita ,  Jose Marcio Vieira Dias Filho ,  Marcos Vinicius Campos ,  Emerson Freitas

发明人： Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Alvaro Vito Polati de Souza ,  Eduardo da Silva Martins ,  Marco Tulio Sguerra Vita ,  Jose Marcio Vieira Dias Filho ,  Marcos Vinicius Campos ,  Emerson Freitas

IPC分类号： G05D1/06

CPC分类号： G05D1/0833

摘要： A flight control system moves elevators according to a pilot command summed with an automatic command. The flight control system monitors a set of flight parameters to determine if the flight vehicle is operating inside a permitted envelope. The flight controls system incorporates automatic protections thru the automatic elevator command if the flight vehicle is close to its envelope limits. The exemplary illustrative non-limiting implementation herein provides automatic protections in order to protect the flight vehicle from low speeds, high attitude, stalls and buffetings.

摘要翻译： 飞行控制系统根据与自动命令相加的飞行员指令移动电梯。 飞行控制系统监视一组飞行参数，以确定飞行器是否在允许的信封内操作。 飞行控制系统通过自动升降机命令包含自动保护，如果飞行器接近其信封限制。 这里的示例性说明性非限制性实施例提供自动保护，以便保护飞行器辆免受低速，高姿态，档位和冲击。

公开(公告)号：US20100217460A1

公开(公告)日：2010-08-26

申请号：US12518361

申请日：2007-12-11

申请人： Alvaro Vitor Polati De Souza ,  Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Jerome Klein ,  Lauro Rocha Borges ,  Reneu Luiz Andrioli, JR. ,  Luciano Tury Pastorini ,  Marco Paulo Fonseca

发明人： Alvaro Vitor Polati De Souza ,  Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Jerome Klein ,  Lauro Rocha Borges ,  Reneu Luiz Andrioli, JR. ,  Luciano Tury Pastorini ,  Marco Paulo Fonseca

IPC分类号： G05D1/06 ,  G06F19/00

CPC分类号： G05D1/0676 ,  G05D1/08 ,  G05D1/0808

摘要： A flight control system commands drag devices such as flight spoilers according to pilot or autopilot longitudinal command. Furthermore, the flight control system monitors a set of flight parameters to determine whether the aircraft is operating inside the permitted safe envelope, hence, incorporating envelope automatic exceeding disengagement. This invention allows the aircraft to descend in a steeper glide path than the 3° used in the normal approach, while keeping speeds unchanged.

摘要翻译： 飞行控制系统根据飞行员或自动驾驶仪纵向命令来命令拖动装置，例如飞行扰流板。 此外，飞行控制系统监视一组飞行参数，以确定飞行器是否在允许的安全信封内操作，因此，将信封自动超出分离。 本发明允许飞行器以比正常进近中使用的3°更陡的滑行路径下降，同时保持速度不变。

公开(公告)号：US4879643A

公开(公告)日：1989-11-07

申请号：US122780

申请日：1987-11-19

申请人： Abhijit J. M. Chakravarty ,  Dagfinn Gangsaas ,  John B. Moore

发明人： Abhijit J. M. Chakravarty ,  Dagfinn Gangsaas ,  John B. Moore

IPC分类号： G05B13/02

CPC分类号： G05B13/021

摘要： An output vector produced by a plant in response to an input vector is filtered by a plurality of bandpass filters, each filter having a different pass band. A filtered output vector from each filter is provided as input to a separate adaptive feedback controller, and feedback vectors produced by the separate controllers are summed to provide the input vector to the plant. Each adaptive feedback controller continuously identifies an open-loop transfer function of the plant characterizing a particular frequency band of plant operation, and continuously adjusts its own open-loop transfer function so that the poles of the closed-loop transfer function of the plant for that particular frequency mode of operation are assigned to constant stable values despite changes in the open-loop transfer function of the plant.

摘要翻译： 由植物响应于输入矢量产生的输出矢量被多个带通滤波器滤波，每个滤波器具有不同的通带。 提供来自每个滤波器的经滤波的输出矢量作为单独的自适应反馈控制器的输入，并且将由分离的控制器产生的反馈矢量相加以将输入矢量提供给工厂。 每个自适应反馈控制器连续地识别表征设备操作的特定频带的设备的开环传递函数，并且连续地调整其自身的开环传递函数，使得该工厂的闭环传递函数的极点 尽管工厂的开环传递功能发生了变化，特定的频率操作模式被分配给恒定的稳定值。