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- 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。
- 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。
- A robust midcourse guidance law based on the zero effort miss is designed for the middle flying stage of exo-atmospheric intercept with the fuel-exhaustion-shutoff solid engine. 摘要针对大气层外拦截中段采用耗尽关机固体燃料发动机的情况,设计了基于零控脱靶量的鲁棒中制导律。
- 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. 摘要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。
- The anti-ship missile is launched from a variety of different height, and under the control of this midcourse guidance law it can successfully realize the large space variable trajectory. 反舰导弹从各种不同的高度进行发射,在该中制导律的控制下均能成功地实现大空域变轨弹道。
- MIDCOURSE GUIDANCE LAW BASED ON NEURAL NETWORK 基于神经网络的中制导律
- STUDY OF OPTIMAL MIDCOURSE GUIDANCE LAW IN COMBINED GUIDANCE 用于复合制导的最优中制导律研究
- Midcourse Guidance Law for an Exoatmospheric Interceptor 大气层外拦截弹中段制导方法研究
- An Engineering Implementation Method of an Optimal Midcourse Guidance Law Using Neural Network 一种神经网络最优中制导规律的工程实现方法
- A Midcourse Guidance Law for an Exo-Atmospheric Interceptor with Fuel Exhaustion Shutoff Motor 大气层外拦截弹中段耗尽关机制导律
- Derivation and simulation of a suboptimal midcourse guidance law for air-launched cruise missile 一种次优空射巡航导弹中制导律的推导与仿真
- Variable Structure Midcourse Guidance Law with Angle Constraint for Anti-Ship Missile 带落角约束的反舰导弹变结构中制导律研究
- midcourse guidance law 中制导律
- 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。
- Like JSOW-C, the estimated $700,000-plus JASSM has an imaging infrared terminal seeker in addition to its GPS-IMU midcourse guidance. 如JSOW-C,这枚造价高达70万美元的JASSM,除了以GPS-IMU导航之外,它也有一套造影红外线终点搜索器。
- To improve the capture probability,the hand-over point of anti-ship missiles between midcourse guidance and terminal guidance was analyzed. 为了提高对目标的捕捉概率,研究了反舰导弹中末制导交班点的选择问题。
- 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。
- The majority of the flight is flown using midcourse guidance, during which the missile makes slight adjustments to its trajectory allowing it to reach the vicinity of the target. 飞行的主要阶段使用的是中段制导,在此阶段制导系统不断微调导弹的飞行轨迹使其到达目标附近。
- Theory of SQP was introduced.The dynamic optimization was transformed into static parameter optimization.The simulation was carried to solve the optimal midcourse guidance. 介绍了SQP算法的理论基础,把动态优化问题转换成SQP可以应用的静态参数优化问题,针对飞行器中段制导这一具体实例进行了数字仿真。
- Simulation process shows that the SQP is efficient to solve the optimal midcourse guidance, quite flexible compared with other optimum methods, and applicable in engineering application. 仿真过程表明,SQP可以高效地求解最优中制导律问题,与其它优化算法相比具有灵活性,工程上具有一定的应用价值。