This paper deals with the modelling and stability analysis of the Automatic Flight Control systems for a Ballistic Missile using Matlab. The Root Locus Analysis of the System is programmed in Matlab for four different transfer functions corresponding to different Aerodynamic Coefficients for the Vanguard...
A modest number of quantities can be interactively plotted on the Interface but the complete trajectory can be saved as either an Excel or Matlab file for further analysis. The trajectory can also be directly displayed in Google Earth for visualization. The GUI can be used to optimize pitch-...
建立火控弹道的数学模型,运用MATLAB软件对该数学模型进行计算分析,得出了弹丸射程与转数之间的关系,以及弹丸初速、射角变化对转数和射程关系的影响。更多例句>> 2) rocket trajectories 火箭弹弹道 例句>> 3) missile path,missile trajectory 导弹弹道<火>4...
6.Modeling and Simulation on Multi-Rigid Body Trajectory of Missile with Parachute Flying at Minimum Altitude基于MATLAB的低空伞弹弹道建模与仿真 7.Verification and Validation of Controlled Trajectory for Guided Air Ammunition制导航空弹药有控弹道的校核和验证 8.Ned to attack targets between long-range and...
Multidisciplinary integrated design of long-range ballistic missile using PSO algorithm In the case of the given design variables and constraint functions, this paper is concerned with the rapid overall parameters design of trajectory, propuls... X Zheng,Y Gao,W Jing,... - 《系统工程与电子技术...
The missile trajectory is shown in Figure 5. Figure 5. Missile flight trajectory. To prove the high performance of the new integrated navigation system, a simulation is done only under the condition of the Gaussian white noises. Compared with the traditional integrated mode, the position and th...