发明名称 |
METHOD FOR DETERMINING A GUIDANCE LAW FOR OBSTACLE AVOIDANCE BY AN AIRCRAFT, RELATED COMPUTER PROGRAM PRODUCT, ELECTRONIC SYSTEM AND AIRCRAFT |
摘要 |
This method for determining an obstacle avoidance guidance law for an aircraft is implemented by a system for determining said guidance law. The aircraft comprises a collision avoidance system adapted to detect a collision risk with the obstacle and said determination system. This method comprises determining (110) one or more set points from among flight path angle and speed set points (VZ_consigne, IAS_consigne), at least one set point (VZ_consigne) depending on at least one vertical speed limit value, at least one set point (VZ_consigne) comprising a vertical component in a vertical direction, each limit value being provided by the collision avoidance system following the detection of a collision risk with the obstacle(s); and computing (160) the avoidance guidance law as a function of the determined set points. During the determination step, at least one determined set point (IAS_consigne) comprises a longitudinal component in a longitudinal direction perpendicular to the vertical direction. |
申请公布号 |
CA2881545(A1) |
申请公布日期 |
2015.09.04 |
申请号 |
CA20152881545 |
申请日期 |
2015.02.09 |
申请人 |
THALES |
发明人 |
CLAYBROUGH, MATTHIEU;COLONNA, FRANCOIS;RIEDINGER, MARC |
分类号 |
B64C19/02;B64C13/16;B64D31/06;B64D47/00 |
主分类号 |
B64C19/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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