Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations

Sedelnikov A. V.; Potienko K. I.

首页> 外文期刊>International Review of Aerospace Engineering >Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations

【24h】

Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations

机译：主动控制微加速度过程中航天器可控性降低的分析

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

There is viewed the problem of reduction of controllability of spacecraft due to increase of inertia moment of spacecraft during conducting of active control over microacceleration level on the operational stage. Additional fuel stores, which are necessary for realization of spacecraft orbital orientation, are estimated. Recommendations to reduce influence of the phenomenon on effective running of system for orientation and control of spacecraft motion are given.

机译：在运行阶段进行微加速度水平的主动控制时，由于航天器的惯性矩增加，导致航天器的可控性降低的问题被观察到。估算了实现航天器轨道定向所需的其他燃料存储。提出了减少现象对航天器运动方向和控制系统有效运行的影响的建议。

著录项

来源
《International Review of Aerospace Engineering》 |2017年第3期|160-166|共7页
作者
Sedelnikov A. V.; Potienko K. I.;
展开▼
作者单位

Samara National Research University, Samara, Russian Federation;

Samara National Research University, Samara, Russian Federation;

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类
关键词
Active Control; Controlled Motion Of Spacecraft; Microacceleration Level;

机译：主动控制;航天器的受控运动;微加速度等级;

相似文献

外文文献
中文文献
专利

1. Fast Analysis of Onboard Measurements of the Earth Magnetic Field for the Purpose of Microaccelerations Decrement on Board of the "AIST" Small Spacecraft During its Uncontrolled Orbital Flight [J] . A. V. Sedelnikov International Review of Aerospace Engineering . 2018,第2期

机译：快速分析“ AIST”小型航天器在其不受控制的轨道飞行过程中以微加速度减小为目的的机载地球磁场测量
2. Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements [J] . Sedelnikov A. V. Microgravity science and technology . 2016,第5期

机译：具有弹性结构元素的航天器姿态控制发动机的运行引起的微加速度建模
3. Problems in Formation and Control of a Required Microacceleration Level at Spacecraft Design, Tests, and Operation [J] . A. I. Belousov, A. V. Sedelnikov Russian Aeronautics . 2014,第2期

机译：在航天器设计，测试和操作中形成和控制所需的微加速度级别的问题
4. Variable Emittance Skins for Active Thermal Control in Spacecraft Based on Conducting Polymers, Ionic Liquids and Specialized Coatings [C] . Prasanna Chandrasekhar, Brian J. Zay, Scott Barbolt, Symposium on New Frontiers in Space Propulsion Sciences . 2010

机译：基于导电聚合物，离子液体和专业涂料的航天器中的可变射精皮肤用于航天器中的主动热控制
5. MANEUVER AND CONTROL OF FLEXIBLE SPACECRAFT (VIBRATION, THREE-DIMENSIONAL, ACTIVE-CONTROL, NONLINEAR, PERTURBATION). [D] . QUINN, ROGER DENNIS. 1985

机译：灵活的航天飞机的操纵和控制（振动，三维，主动控制，非线性，扰动）。
6. Conducting a pilot randomized controlled trial of community-based mindfulness-based stress reduction versus usual care for moderate-to-severe migraine: protocol for the Mindfulness and Migraine Study (MM) [O] . Alice Pressman, Heather Law, Robert Stahl, 2019

机译：针对中度至重度偏头痛进行以社区为基础的正念为基础的压力减轻与常规护理的随机对照试验：正念和偏头痛研究（M＆M）的方案
7. Vehicle Idling Vibration Reduction Using Electric Machine Active Torque Control. (2nd Report, Influence of Control Torque Waveform on Control). [O] . Yuzo Kadomukai, Makoto Yamakado 1993

机译：使用电机主动扭矩控制的车辆空转减振。（第2次报告，控制扭矩波形对照的影响）。
8. Multidisciplinary analysis of actively controlled large flexible spacecraft [R] . Cooper, Paul A., Young, John W., Sutter, Thomas R. 1986

机译：主动控制大型柔性航天器的多学科分析

Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations

摘要

著录项

相似文献

相关主题

期刊订阅