Chinese translation for "midcourse guidance"
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- 飞行中段引导
中程制导
Related Translations:
- Example Sentences:
| 1. | Study of handing over between midcourse guidance and terminal guidance for multi - purpose missiles
多用途导弹中末段交班研究 | | 2. | The proposed algorithm can be used in the design of pure inertial midcourse guidance scheme
该算法可用于纯惯性中制导方案设计。 | | 3. | The simulation result shows that the influence of the midcourse guidance based on the inertial navigation on the missile ' s impact point is remarkable
仿真结果表明，纯惯导中制导对洲际导弹落点精度影响比较大。 | | 4. | Forth , this thesis also had made a preliminary discussion on the integrated guidance system of air - to - air missile beyond visual range air combat and made deep research on the midcourse guidance stage , thus we obtained an extremely useful conclusion .
本文还对空空导弹超视距攻击的复合制导体制做了一个初步的探讨,并对其中的中制导阶段进行了深入研究,得到了一个十分有用的结论:即中制导阶段导弹发动机的最优推力方向实际上应该是关于时间的线性函数。 | | 5. | Based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application
为满足实际作战的要求，基于最优控制理论和奇异摄动方法，提出了一种可保证中远程空地导弹快速爬升到最优高度的中制导律.它由变系数最优爬升控制，最小能量巡航控制和最小能量下滑控制组成.为了减小爬升段控制对下滑段的影响，提出了一种新的控制逻辑.最后针对某型空地导弹进行了仿真.结果表明，该中制导律较好地满足了中远程空地导弹在中制导段的要求.本文的研究结果具有较好地工程参考价值 | | 6. | In this paper . the question of compound guidance about mid - long range air - to - air missle to be considered . the main contributions are as follows : first , two midcourse guidance laws are given . that is optimally predictable pn micourse guidance , which is suitable for middle range missle , and singularly perturbed midcourse guidance . which is suitable for long range missle guidance ; then two terminal guidance laws are given . that is variable structure guidance , which is suitable for passive radar guidance . and optimal guidance which is suitable for active radar guidance ; and then the error sourses of hand - off are researched , the hand - off law is given at the time ; fmally , the midcourse guidance laws and terminal guidance laws are tested by simulation , and the whole trajectory simulation are given through hand - off law , and the results are satisfied
主要工作如下：首先研究了用于中远程空空导弹复合制导的两种中制导律，即用于中程导弹的最优预测比例导引中制导律和用于远程导弹的奇异摄动中制导律，它们均有很好的中制导性能，能够满足中末制导的交班要求；接着研究了两种末制导律，即用于被动雷达末制导的变结构制导律和用于主动雷达导引头的最优末制导律，均适用于复合制导末制导段；然后分析了中末制导的交班误差源，讨论了用于复合制导的交接律；最后通过仿真，验证了提出的中制导律和末制导律，结合提出的交接规律，在不同的情况下对中末制导段弹道进行了仿真验证，结果证明文中提到的中末制导律能够达到性能指标要求。 | | 7. | Abstract : based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application
文摘:为满足实际作战的要求，基于最优控制理论和奇异摄动方法，提出了一种可保证中远程空地导弹快速爬升到最优高度的中制导律.它由变系数最优爬升控制，最小能量巡航控制和最小能量下滑控制组成.为了减小爬升段控制对下滑段的影响，提出了一种新的控制逻辑.最后针对某型空地导弹进行了仿真.结果表明，该中制导律较好地满足了中远程空地导弹在中制导段的要求.本文的研究结果具有较好地工程参考价值 | | 8. | Taking intercontinental ballistic missiles as objects under research , and based on the analysis of the influence of accelerometer measurement error and gyroscope excursion error on the apparent acceleration , the error transfer model of the inertial system in a midcourse guidance segment for velocity and location is given , and the pure inertial navigation guidance error is computed with the given imu error coefficient deviations
摘要针对洲际弹道导弹，在分析加速度计测量误差和陀螺漂移误差对导弹视加速度影响的基础上，给出了中制导段惯性系统对速度和位置的误差传递模型，对给定的惯组误差系数偏差进行了纯惯性导航制导误差计算。 |
- Similar Words：
- "midcourse correction engine" Chinese translation, "midcourse data" Chinese translation, "midcourse decoy" Chinese translation, "midcourse discrimination" Chinese translation, "midcourse flight" Chinese translation, "midcourse guidance simulator" Chinese translation, "midcourse homing" Chinese translation, "midcourse intercept system" Chinese translation, "midcourse maneuver" Chinese translation, "midcourse motor" Chinese translation
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