航天器对接

航天器对接试验台三轴姿态调整锁定机构研究

Three-freedom attitude adjusting and locking mechanism of spacecraft docking test table

航天器对接系统中相对运动参数测量的计算机视觉方法

A Computer Vision Approach to Relative Motion Measurement in Spacecraft Docking System

周边式对接机构对接动力学仿真本文以交会对接仿真系统研制为背景，研究了带有周边式对接机构的航天器对接动力学问题，并开发了对接动力学仿真系统（DDSS）。

By employing the development of the RVD simulation system as the research background , the main work of this dissertation is to study the docking dynamics of spacecraft with Peripheral Docking Mechanisms and to develop the docking dynamics simulation system ( DDSS ) .

航天器对接接触过程撞击动力学分析

Contact-impact dynamic analysis of spacecraft in the course of space docking

某型航天器对接控制过程的建模与仿真研究

Study on Modeling and Simulation of Docking Control Process of Some Spacecraft

航天器对接六维试验台内装式重力平衡技术

Gravity balance technique installed on six-freedom spacecraft docking test table

时变不确定约束的航天器对接动力学分析第一部分运动学约束方程

Docking dynamics analysis of spacecraft with varying indeterminate constraint

基于虚拟样机的航天器对接转动模拟装置仿真研究

Spacecraft Docking Rotating Simulator Based on Virtual Prototype

航天器对接相对位置姿态自主测量方法研究

Relative position-and-attitude self-measuring for spacecrafts docking

航天器对接过程的动力学建模

Dynamic Modeling of Spacecraft Docking Process

我设计的接口卡后来被研究所的航天器对接模拟系统所使用。

The interface card that I designed was later added to NSRO 's Spacecraft Interface Simulator ( SIS ) systems .

确定接触点问题是航天器对接过程中接近与接触阶段的仿真的关键问题。

One of the key problems of two spacecraft 's docking simulation in the period from approach to first contact is to determinate the contact points .

针对地面航天器对接动力学全物理仿真试验台，提出采用质量惯量模拟技术模拟航天器的质量、惯量特性，以便灵活的适应不同吨位航天器对接试验。

Technique of mass and inertia simulating is proposed to simulate spacecraft 's mass and inertia on a ground physical docking dynamics simulation test bed , which makes the docking test bed simulate different mass spacecraft docking .

近年来，应用于火箭发动机推力试验、飞机试飞试验、航天器对接模拟试验及风洞试验等领域的大量程六维力传感器，成为急需的高科技产品。

Recently , the wide-range six-component force / torque sensor becomes the urgent need high-tech product , which can be used in thrust testing of rocket engines , flight testing of airplane , testing of spacecraft docking simulation and wind tunnel .

对航天器对接试验台的动力学建模问题进行了研究，建立了接触点的动态变约束方程、对接碰撞力模型，并应用牛顿-欧拉方法提出了五自由度下捕获阶段运动学模型。

The dynamic model of spacecraft docking test table was studied . The equations with dynamic constrain in contact point and contact force model during the docking process were built , and five-freedom kinematic model of capturing process was built by Newton-Euler method .

GPS在航天器交会对接中的应用研究

The Application of GPS in the RVD

设计了GPS相对导航在航天器交会对接中应用的两种方案；

Two scenarios of applying GPS relative navigation for spacecraft RVD ( Rendezvous and Docking ) are proposed .

GPS用于航天器交会对接的方案与模糊度OTF解算研究

Scenarios of Applying GPS for Spacecraft RVD and the Study of Applying OTF Ambiguity-Resolution Method

航天器交会对接位姿视觉测量迭代算法

An iterative method for vision-based relative pose parameters of RVD spacecrafts

航天器交会对接发射时间的选择与确定

Selection and Determination of the Launch Time for Spacecraft Rendezvous and Docking

通过模拟件的调整，试验台可以实现不同航天器的对接动力学仿真试验。

The test bed can simulate different spacecraft docking dynamic tests by adjusting the simulator .

基于对偶四元数的航天器交会对接位姿视觉测量算法

Algorithm of Vision Measure for Relative Position and Pose of RVD Spacecrafts Based on Dual-quaternion

实验表明，该信号处理机可以满足空间航天器交会对接的要求。

Tests indicate that the signal processor can meet the requirements of Rendezvous and Docking .

研究带周边式对接机构的航天器在对接捕获过程中的缓冲动力学行为。

The dynamic process of capturing and docking space vehicles with the androgynous peripheral docking mechanism is studied .

周边式对接机构航天器的对接动力学仿真（第1部分）&运动学约束方程

Docking Dynamics Simulation of Spacecraft with Peripheral Docking Mechanism ( Part : I ) & Equation of Kinematics Constrained

在进行航天器交会对接制导方案设计时，必须考虑在误差情况下航天器交会任务的实现。

While guidance project of the spacecrafts ' rendezvous is designed , completion of rendezvous under error condition is considered .

本文介绍了将智能控制方法用于航天器交会对接段的轨道控制。

The method of intelligent control applied to the orbital control of rendezvous and docking phase of spacecraft is presented in this paper .

对航天器交会对接最终逼近段，给出姿态运动学方程统一形式以及相对姿态动力学方程；

Motion equations of relative attitude between the target and chase spacecraft were elaborated for the final approach phase of spacecraft rendezvous and docking .

激光雷达具有重要的军事应用价值和民用价值，主要应用于军事侦察、军事气象、航天器交会对接和地球科学研究方面。

Lidar is very important in military field and civil field , which includes military reconnaissance , military weather service , spacecraft dockage , research of earth science , and so on .

仿真结果表明通过滤波，激光雷达能够为航天器交会对接提供足够精度的相对位置和相对速度信息。

The results of simulation indicate that working together with the EKF , ladar can provide the information of relative position and relative velocity with sufficient accuracy for the spacecrafts rendezvous and docking .