Research on Angular Motion Characteristics and Stability of Trajectory-Corrected Rocket Projectile with Isolated Rotating Tail Rudder

Table 2

Projectile body and aerodynamic parameters.

Parameters	Values
m (kg)	6
C1 (kg·m^2)	5.01e − 3
bx (m^−1)	4.28e − 4
bz (1)	3.5e − 7
kxz2 (m^−1)	2.5e − 4
kz (m^−2)	3.47e − 2
δN (rad)	4.01e − 2
A (kg·m^2)	2.48e − 1
C2 (kg·m^2)	5.04e − 4
by (m^−1)	8.94e − 3
kxz1 (m^−1)	1.25e − 4
ky (m^−1)	−9.01e − 3
kzz (m^−1)	2.76e − 2
δM (rad)	8.11e − 2