The Suppression of Triangle Size Effect in Spaced Antenna Wind Measurements

Based on the current state of the spacecraft, make the transfer nominal terminal as control target, the Lambert algorithm was used to re-plan the transfer orbit, and impose appropriate controls make the spacecraft entering the transfer orbit.

该方法根据航天器当前状态，以转移终端标称状态为控制目标，采用Lambert算法重新规划转移轨道，并施加合适控制使其进入转移轨道。

互联网摘选

spacecraft Into the geosynchronous transfer orbit speed of 10.25 kilometers requirements/ s;

航天器进入地球同步转移轨道运行所需速度为10.25公里／秒；

互联网摘选

Nonlinear control of large-angle attitude maneuvers for flexible spacecraft with angular momentum transfer

具有角动量存贮挠性飞行器大角度姿态机动的非线性控制

互联网摘选

Spacecraft needs not only transfer data to the ground, but also share the information with each other.

航天器不仅需要将数据实时地传输到地面，而且需要与其他航天器实现信息共享。

互联网摘选

Robust Attitude Control of Flexible Liquid Spacecraft under Fast Orbit Transfer

轨道快速机动期间的姿态鲁棒稳定控制方法研究

互联网摘选

Long March 3 ( LM-3) is a three-stage launch vehicle, primarily intended for sending spacecraft into Geosynchronous Transfer Orbit with the GTO capacity of l.

“长征三号”运载火箭是三级火箭，主要用于发射地球同步轨道有效载荷，运载能力为1.5吨。

互联网摘选

Study on the Minimal Energy Maneuvering Control of a Rigid Spacecraft with Momentum Transfer

刚体航天器的最小能量姿态机动最优控制研究

互联网摘选

By building the LEO satellite network, it is easy for spacecraft to transfer and share data. However the network access method is one of challenges of the LEO satellite network.

通过建设LEO卫星网，容易实现航天器的数据传输与共享，但是航天器的网络接入是研究难点之一。

互联网摘选

By choosing controllers, sensors and exciters, many experiment strategies can be realized, including the dynamic characteristics of the rigid-flexible-fluid coupling multi-body spacecraft, the large angle maneuver of the center body of spacecraft and multi-target attitude tracking control, and so on.

通过选择不同控制、测量、激振组合，该实验系统可以用于研究刚弹液耦合系统的动力学特性、中心体姿态机动及多目标姿态跟踪控制等多类问题。

互联网摘选

With the development of missile, Satellites, spacecraft, moderate precise tracking radar can not meet the tracking measurement requirements of weapons systems gradually.

随着导弹、卫星、航天飞行器的出现，中等精度的跟踪雷达逐渐满足不了武器系统的跟踪测量要求，因而催生了20世纪50年代诞生的精密跟踪雷达。

互联网摘选

Spacecraft Adaptive Attitude Tracking and Stable Control with Variable Speed Control Moment Gyroscopes

采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究

互联网摘选

At the same time, it avoids the chattering phenomenon caused by discontinuity in the variable structure control and fulfills the control mission of spacecraft attitude tracking time-varying signal with good robustness.

实现了航天器姿态跟踪时变参数的控制，并具有较强的鲁棒性。

互联网摘选

For rigid spacecraft attitude tracking system with uncertain inertia matrix and external disturbances, an adaptive sliding mode approach is presented.

针对存在不确定惯量矩阵和外干扰的刚体航天器姿态跟踪系统，提出了一种自适应滑模控制方法。

互联网摘选

Design of higher-order sliding mode controller for rigid spacecraft attitude tracking maneuver

刚体航天器姿态跟踪的高阶滑模控制器设计

互联网摘选

Nonlinear Robust Adaptive Control for Spacecraft Attitude Tracking System

航天器姿态跟踪系统的非线性鲁棒自适应控制

互联网摘选

Autonomous navigation will simplify ground system on spacecraft tracking and routine orbit determination.

通过减少地面系统日常的轨道确定工作和跟踪任务，自主导航可以简化航天器的地面系统。

互联网摘选

Detection of Outliers from Spacecraft Tracking Data using GP-RBF Network

GP-RBF网络应用于飞行器外测数据野值实时剔除

互联网摘选

Research Based on Nonlinear Filtering for Reentry Spacecraft Tracking

基于非线性滤波的再入飞行器跟踪研究

互联网摘选

Statistical diagnosis method for outliers from spacecraft tracking data

靶场外测数据野值点的统计诊断技术

互联网摘选

Study of Rationality Checking Method for Spacecraft Tracking Data

合理性检验的方法研究定量刀口检验研究

互联网摘选