1.
The Study of Reentry Guidance Law Based on CMAC Network
基于CMAC网络的飞行器再入制导研究
2.
Design of Predictor-Corrector Reentry Guidance Law for Lunar Mission Spacecraft
探月飞船预测-校正再入制导律设计
3.
Reentry guidance law design for RLV based on predictor-corrector method
基于预测校正方法的RLV再入制导律设计
4.
Adaptive Reentry Guidance Law for Onboard Changing Attack Objective
具备目标重定向能力的自适应再入制导律
5.
Study of Reentry Guidance of Maneuverable Weapon Based on Neural Network
基于神经网络的轨道武器再入制导研究
6.
The predictor-corrector reentry guidance algorithm for reusable launch vehicles was studied.
研究了可重复使用运载器的预测－校正再入制导方案。
7.
Analysis and Prediction of Reentry Error for Reentry Maneuvering Warhead With Integrated Navigation System
复合制导再入机动弹头再入误差分析
8.
DESIGN OF GUIDANCE AND CONTROL SYSTEM FOR HIGH SPEED REENTRY AEROCRAFT
高速再入飞行器的制导与控制系统设计
9.
Guidance Law of Maneuvering Reentry Warhead Based on Stochastic Variable Structure Control Theory
基于随机变结构控制理论的再入弹头制导律
10.
Study of Missile Reentry Dynamic Decoupling Control Based on Variable Structure Robustness Compensating
动态解耦和变结构鲁棒补偿的导弹再入控制
11.
Analytical Predictive Guidance for Space-to-ground Kinetic Weapon in Reentry
天基对地打击动能武器再入解析预测制导技术
12.
Application of a new guidance law in moving-mass reentry vehicle
新型制导律在变质心再入飞行器中的应用
13.
Reentry Trajectory Guidance Design for Hypersonic Vehicles Based on CMAC Network
基于CMAC网络的飞行器再入标准轨道制导
14.
An Optimal Guidance Law for Reentry Warhead Base on Angular Velocity
一种基于角速率的再入弹头最优制导律
15.
multiple independent reentry vehicle
多弹头分导再入飞行器
16.
Theory of Predictive Guidance with Application to Reentry and Exoatmospheric Interception;
预测制导理论在飞行器再入与大气层外拦截中的应用
17.
MIRV (multiple independently targeted reentry vehicle)
多弹头分导再入飞行器（多弹头导弹）
18.
Based on the inertial guidance instrument error model, the model of reentry point's parameters is established in this paper.
基于惯性制导工具误差模型,推导出存在工具误差时的再入点运动参数模型。