Research Article
A Novel Vibration Control System Applying Annularly Arranged Thrusters for Multiple Launch Rocket System in Launching Process
Figure 10
Simulated results of the elevation part in launching process for the 14th rocket under Condition 2: (a) the yawing angular velocity and (b) the pitching angular velocity. The blue dots indicate the action of the AAT.
(a) |
(b) |