The simulation results shows that lateralattitude control system has good control performance and the auto-trim control strategy plays a effective role.
仿真验证结果表明，抗不确定干扰的横侧向姿态控制回路控制性能良好，自动配平控制策略能有效发挥作用。
2
A launch vehicle with lateral jet as its attitude control mechanism during ascending stage was proposed.
建立了运载器起飞段侧喷流直接力姿态控制模型。
3
Moving the elevators out of their faired position causes the airplane to change the pitch attitude about the lateral axis.