公开(公告)号：US20130138274A1

公开(公告)日：2013-05-30

申请号：US13304979

申请日：2011-11-28

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

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

IPC分类号： G05D1/06

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：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。