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Invention Publication
CN110308738A 用于控制飞行器的轨迹的方法和系统及飞行器 无效 - 撤回

用于控制飞行器的轨迹的方法和系统及飞行器
Abstract:
本发明涉及用于控制飞行器的轨迹的方法和系统及飞行器。控制系统(1)包括：位置确定模块，该位置确定模块被配置成确定安全位置(PS)，该安全位置与尾随飞行器(AC2)在保持在编队飞行(F)中时不经受前导飞行器(AC1)所产生的右涡流(V1)和左涡流(V2)的效应的位置相对应；保护模块，该保护模块被配置成在尾随飞行器所包括的机翼尖端位于如下位置时使尾随飞行器转移至并保持在安全位置：所具有的右涡流特征标记小于或等于第一预定特征标记的位置；或所具有的左涡流特征标记大于或等于第一预定特征标记的位置；或所具有的右涡流特征标记大于或等于第二预定特征标记的位置；或所具有的左涡流特征标记小于或等于第二预定特征标记的位置。
Abstract(English):

System and method for controlling trajectory of an aircraft. The control system includes a position determination module to determine a safety position corresponding to a position in which a follower aircraft is not subject to effects of the right-hand and left-hand vortices generated by a leader aircraft while remaining in formation flight, a protection module to convey and to maintain the follower aircraft to/in the safety position when the follower aircraft comprises a wing tip located in a position that has a right-hand vortex signature that is less than or equal to a first predetermined signature or that has a left-hand vortex signature that is greater than or equal to the first predetermined signature or that has a right-hand vortex signature that is greater than or equal to a second predetermined signature or that has a left-hand vortex signature that is less than or equal to the second predetermined signature.

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