您要查找的是不是:
- Based on the pursuit guidance law and the proportional guidance law, a new guidance law is proposed for space intercept. 摘要基于追踪导引律和比例导引律,提出了一种新的空间拦截末制导律。
- The capability that the naval crotale system with the relative proportional guidance law attacks a maneuverable target near the meeting point was discussed. 讨论“海响尾蛇”导弹在临近遭遇点时采用相对比例导航制导律对付机动目标的能力问题。
- optimal proportional guidance law 最优比例制导
- optional proportional guidance law 最优比例导引法
- A MODIFIED PROPORTIONAL GUIDANCE LAW FOR MEDIUM AND LONG-RANGE BTT AIR-DEFENCE MISSILE 中远程BTT防空导弹的一种修正比例导引规律
- Proportional guidance law 比例导引规律
- Proportional navigation(PN)is used as the guidance law for the guided projectile on which SINS/GPS and terminal homing system are adopted. 针对采用SINS/GPS和末端寻的复合制导的制导炮弹,采用比例导引作为中制导和末制导的导引规律。
- This paper studies the implementation of intercepting satelliteby using proportional guidance in the midcourse. 运用比例导引实现对目标卫星拦截的中制导方法进行了研究。
- The computational results show that the transform condition with higher precision to the terminal guidance by using proportional guidance in the midcourse is guaranteed. 计算结果表明,在中段运用比例导引可保证向末制导转换时有较高精度的转换条件。
- Proportional Navigation guidance law (PN) 比例导引律
- Proportional navigation guidance law 比例导引
- Simulation results show that the performance of the designed guidance law is superior to that of TPN and APN, and close to that of OPG. 仿真研究表明,该导引律性能优于TPN,APN,接近OPG。
- In this paper, the precise initial guidance law based on velocity gain guidance and the state transition matrix for orbit interception were proposed. 摘要对于轨道拦截问题,给出了一种基于速度增益制导和状态转移矩阵的精确初制导方法。
- The miss distance caused by guidance method error and the effects of perturbation are compensated in this initial guidance law. 该初制导方法能补偿制导方法误差和轨道摄动对拦截脱靶量的影响。
- A midcourse guidance law based on zero effort miss forecasting is presented for intercepting a high-speed target in three-dimensional space. 针对三维空间内的高速飞行目标,提出了一种基于预测零控脱靶量的中制导段导引方法。
- semi-active laser proportional guidance 半主动激光比例导引
- typical proportional guidance regulation 经典比例导引规律
- Abstract Optimal guidance law for a torpedo impacting vertically on a maneuvering evader in three dimensions is studied. 摘要 本文研究了三维空间中鱼雷垂直命中机动目标的最优导引律设计问题。
- Applying the optimal guidance law in this paper to a reentry warhead, this optimal control law was proved effective through computer simulation. 将此最优制导算法应用到某型再入弹头,通过计算机仿真验证了算法的正确性。
- A variable structure midcourse guidance law with terminal angle constraint is proposed, based on the concept of virtual target. 基于虚拟目标的概念,提出了一种带落角约束的变结构中制导律。