A Control Allocation Method to Reduce Roll-Yaw coupling on Tailless Aircraft
A Control Allocation Method to Reduce Roll-Yaw coupling on Tailless Aircraft
复制标题
无尾飞机减少横滚偏航耦合的控制分配方法
DOI:
10.2514/6.2021-1826
复制
发表时间:
2021
期刊:
影响因子:
--
通讯作者:
Shearwood T
中科院分区:
文献类型:
--
作者:
Shearwood T
影响因子:
2.6
作者:
Thomas R. Shearwood;M. Nabawy;W. Crowther;C. Warsop
通讯作者:
Thomas R. Shearwood;M. Nabawy;W. Crowther;C. Warsop