| 1. | Aerodynamic prediction and analysis for a reentry vehicle with slice - ailerons
配平翼飞行器的气动计算及分析 |
| 2. | Maneuverable reentry vehicle
可操纵返航运载工 |
| 3. | Improving design of reentry vehicle trajectory optimization using direct collocation method
基于直接配点法的再入轨迹优化设计 |
| 4. | Learning classifier system and its application to the aerodynamic shape optimization of reentry vehicle
自适应分类器系统及其在再入飞行器气动布局优化中的应用 |
| 5. | Finally , use the multiple delay model and multiple design point approach to achieve the control law design for the energy management phase of a reentry vehicle
最后利用多重延迟模型和多重设计点( mdm mdp )方法设计了航天器末端能量管理段的控制律。 |
| 6. | The innovation of this dissertation includes presentation of the moving mass control program for the reentry vehicle , the dynamics equation of the reentry vehicle with moving mass
本文的创新之处在于提出了一种新颖的再入机动控制思想,并推导了变质心机动再入体动力学方程。 |
| 7. | The optimization design of aerodynamic shape for reentry vehicles ( asrv ) is a design problem of the complex engineering system , which often involves several subsystems and various parameters
再入飞行器气动布局优化设计是一个复杂的工程系统设计问题，通常包含若干子系统和大量的设计参数。 |
| 8. | Finally , the aerodynamic shape optimization design examples for three kinds of reentry vehicles are implemented , which involve a reentry vehicle with cruciform flaps , a variable - bend reentry vehicle and a crew transfer vehicle
本文的最后，应用智能优化设计系统对带控制舵机动式再入飞行器、可变弯体再入飞行器以及一种载人返回舱气动布局这三类工程问题来进行优化设计。 |
| 9. | Among different movement mode of moving mass , the influence of lateral displacement of the moving mass on the attitude motion of the re - entry vehicle is discussed , the effect of different moving mass ratio and axis position imposing on the attitude of the reentry vehicle is also studied
本论文详细地分析了影响系统姿态的因素,研究了在不同的质量体运动形式下,活动质量体的横向偏移量、质量比、和轴向位置对姿态动力学响应的影响。 |
