| 1. | Is capture region of 3d ideal proportional navigation also the biggest
三维理想比例导引律的捕获区域分析 |
| 2. | Augmented proportional navigation
扩充比例导航 |
| 3. | Study of target acquisition probability for laser - guided bombs with proportional navigation guidance law
激光比例制导航弹对目标的捕获概率分析 |
| 4. | Design and identification on parameters of proportional navigation guidance law with gravity over compensation
带过重力补偿的比例导引制导律参数设计与辨识 |
| 5. | Simulations show that the variable structure guidance law yields much better performance compared to proportional navigation
仿真结果表明，所提出的制导律与比例导引相比有较大的性能改善。 |
| 6. | Like proportional navigation guidance ( png ) , the new guidance law , which utilizes line - of - sight ( los ) measurement only , is simple in implementing
在执行上，变结构制导律仅使用了视线转率测量值，因而和比例导引同样简单。 |
| 7. | The designed robust guidance laws are used to the simulation of air - air missile ' s attack process . the designed robust guidance laws are more valid than the proportional navigation guidance law
与传统的比例制导律相比，所设计的h ’鲁棒制导律效果更好，鲁棒性更强。 |
| 8. | Next , to gain accurate los rate is the key for hit - to - kill since true proportional navigation ( tpn ) is convergent if the initial state between ekv and target is inside the capture region
其次,由于真比例导引本身是稳定的,所以获取一定测量精度的视线角速率是实现成功拦截的关键。 |
| 9. | Simulation studies show that the proposed law in this paper has better guidance accuracy and better dynamic property during pursuit - control processing and it is superior to proportional navigation
仿真结果表明，给出的导引律在攻击机动目标时制导精度高、脱靶量小，导引控制过程具有良好的动态性，性能明显优于传统的比例导引律。 |
| 10. | Two spacecraft ’ s rendezvous technology in coplanar near - earth orbit with maneuvering target , based on the sight coordinate system is presented in this paper . differential games guidance law ( dggl ) and proportional navigation ( pn ) are studied
本论文研究了近地共面轨道两空间飞行器在目标机动下的在轨交会技术,分别对微分对策制导律和比例导引制导律两种制导方法进行了研究。 |
