A Kind of Mixed Reentry Guidance Method for Weapon System of Space-based Attack Ground;
天基对地攻击武器的一种混合再入制导方法研究
This paper introduce the recent development of the spacecraft reentry guidance method in the world.
介绍了国内外航天器再入制导方法领域研究的近期进展,分标准轨道制导法和预测-校正制导法详细剖析了各种再入制导律的设计思路与研究框架,指出了自主性、自适应性和鲁棒性、并且能够适应多任务的新型再入制导方法是目前的研究热点和发展方向。
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。
Entry guidance and trajectory tracking error analysis;
再入制导和弹道跟踪误差分析(英文)
A new reusable launch vehicle(RLV) entry guidance algorithm with ranging technique which only needs to update flight profile parameters was developed and a predictor-corrector entry guidance methodology using Runge-Kutta-Fehlberg method for RLVs combined with trajectory online generation technology was studied.
进一步对两种制导方法进行了比较分析研究,研究认为标准轨道制导与轨道预测制导都是可行的RLV再入制导方案,其有机结合是未来可重复使用跨大气层飞行器再入制导的发展趋势。
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
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
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
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
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
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。
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
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
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
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
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
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
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
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
multiple independent reentry vehicle
多弹头分导再入飞行器
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
MIRV (multiple independently targeted reentry vehicle)
多弹头分导再入飞行器（多弹头导弹）
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。