公开(公告)号：US08165733B2

公开(公告)日：2012-04-24

申请号：US11849501

申请日：2007-09-04

申请人： Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Alvaro Vito Polati de Souza ,  Eduardo da Saiva 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 Saiva 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.

公开(公告)号：US20110054720A1

公开(公告)日：2011-03-03

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： G05D1/08

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：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：US20090062973A1

公开(公告)日：2009-03-05

申请号：US11849501

申请日：2007-09-04

申请人： Fabricio Reis Caldeira ,  Dagfinn Gangsaas ,  Alvaro Vitor 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 Vitor 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： G05D1/08 ,  G06F17/00 ,  G06F7/00

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：US08606437B2

公开(公告)日：2013-12-10

申请号：US13304979

申请日：2011-11-28

申请人： Fabricio Reis Caldeira ,  Marcos Vinicius Campos ,  Reneu Luiz Andrioli, Jr. ,  Wagner de Oliveira Carvalho ,  Dagfinn Gangsaas ,  Eduardo Camelier ,  Daniel Siqueira ,  Lucas Rubiano

发明人： Fabricio Reis Caldeira ,  Marcos Vinicius Campos ,  Reneu Luiz Andrioli, Jr. ,  Wagner de Oliveira Carvalho ,  Dagfinn Gangsaas ,  Eduardo Camelier ,  Daniel Siqueira ,  Lucas Rubiano

IPC分类号： B64C13/00

CPC分类号： G05D1/0676

摘要： A longitudinal control law is designed to optimize the flying qualities when aircraft is set to approach configuration, i.e. when the flap lever is set to the landing position and landing gears are locked down. Under such circumstances, the effort of trimming the aircraft speed can be extremely reduced by the usage of a momentary on-off switch or other control in the sidestick, instead of or in addition to a conventional trim up-down switch, making easier the task of airspeed selection by the pilot. This control law provides excellent handling qualities during approach and landing, with the benefit of not needing or using radio altimeter information in safety-critical applications.

摘要翻译： 纵向控制规律被设计为当飞行器被设置为接近构造时，即当翼片杆被设置到着陆位置并且起落架被锁定时，优化飞行质量。 在这种情况下，可以通过使用瞬时开关开关或旁路中的其他控制来极大地减少飞行器速度的改进，而不是传统的调节上拉开关，也可以简化任务。 飞行员选择空速。 该控制法在接近和着陆期间提供极好的处理质量，有利于在安全关键应用中不需要或使用无线电高度计信息。

公开(公告)号：US09405295B2

公开(公告)日：2016-08-02

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： G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  G06F7/00 ,  G06F17/00 ,  G05D1/06 ,  G05D1/08

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：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。