基于积分反步法的四旋翼飞行器控制设计
郭妍,吴美平,唐康华,王雪莹
Integral back-stepping algorithm for designing the quadrotor aircraft controller
Yan GUO,Meiping WU,Kanghua TANG,Xueying WANG
表1
四旋翼飞行器仿真参数
参数
m(kg)
J
x
(kg.m
2
)
J
y
(kg.m
2
)
J
z
(kg.m
2
)
l(m)
量值
0.6150
0.0154
0.0154
0.0309
0.0305