| 1. | Dynamic simulation based on matlab simulink of sam guidance and control system
的地空导弹制导控制系统动态仿真 |
| 2. | A study of homing missile guidance and control system hardware - in - the - loop simulation
某寻的导弹制导控制系统半实物仿真研究 |
| 3. | According to the requirement of trajectory stability , the quantitative principle of related parameter choosing is presented
从弹道稳定性的要求出发，对制导控制系统相关参数选择的原则给出了定量的结果。 |
| 4. | In section 3 , the rule of air combat countermeasure is given , and the intelligence guidance problem of air combat with reinforcement learning is discussed
在第三章设计了基于q -学习智能空战制导控制，并给出空战对策准则。 |
| 5. | Using the high speed d / a and a / d ics to realize the sampling and realtime control function of the system . 4 . designing the power supply , filter , and other periphery curcuits
对于数字信号处理技术进行了研究，并采用了数字信号处理器tmslf2407a来实现制导控制功能。 |
| 6. | First , the maximum principle is used to generate an optimal guidance law for lunar landing , and the tpbvp is to be solved as a result of the numerical solution for optimal trajectory
文中首先应用极大值原理设计了最优着陆制导控制律，此时求解最优轨迹变成一个两点边值问题( tpbvp ) 。 |
| 7. | Traditional simulation methods of air defense missile weapon system mainly focus on the simulation of control system and guide system , and do not deal with signal receiving and signal processing
经典的防空导弹武器系统仿真主要是制导控制系统的仿真，对信号的接收和处理则没有涉及。 |
| 8. | Simulation result showed that response time of missile was reduced and guidance accuracy was accordingly increased by side jet and aerodynamic compound control manner in terminal guidance
通过仿真研究表明：在末制导阶段，采用燃气动力气动力复合控制方式可提高导弹的快速性，进而提高导弹的制导控制精度。 |
| 9. | Abstract : the method framework of object - oriented simulation are introduced . its concept and basic structure is indicated in detail . by studying on simulation of guide control system of one antiaircraft missile , its existence and importance on study of system simulation are proved
文摘:提出了面向对象仿真方法框架，详细说明了它的概念和基本结构，通过对某型防空导弹制导控制系统的仿真研究，证明了它的合理性和在系统仿真研究中的重要性。 |
