公开(公告)号：US4821981A

公开(公告)日：1989-04-18

申请号：US147066

申请日：1988-01-25

申请人： Dagfinn Gangsaas ,  Daniel C. Norman

发明人： Dagfinn Gangsaas ,  Daniel C. Norman

IPC分类号： B64C13/16 ,  G05D1/06

CPC分类号： B64C13/16 ,  G05D1/0623

摘要： This invention provides a system for enhancing the performance of an aircraft during flight. The aircraft, which includes at least two control surfaces, such as stabilon and trailing edge flaps, includes devices for: generating a signal representative of the optimum normal acceleration from signals representative of the aircraft's flight status, generating a signal representative of the aircraft's actual normal acceleration, comparing the optimum signal to the actual signal, and generating a command to alter the position of either one or both of the aircraft's control surfaces to reduce any differences between the optimum and actual normal acceleration signals.

摘要翻译： 本发明提供了一种用于在飞行中增强飞机性能的系统。 包括至少两个控制表面（例如稳定翼和后缘翼片）的飞行器包括用于：产生代表飞机的飞行状态的信号代表最佳正常加速度的信号的装置，产生代表飞机实际正常的信号 加速度，将最佳信号与实际信号进行比较，并产生改变飞行器控制表面中的任一者或两者的位置的命令，以减少最佳和实际正常加速度信号之间的差异。