首页> 外文OA文献 >A Flight-Path Control of Aircraft Based on Required Acceleration Vector

【2h】

A Flight-Path Control of Aircraft Based on Required Acceleration Vector

机译：基于所需加速度向量的飞机飞行路径控制

代理获取

本网站仅为用户提供外文OA文献查询和代理获取服务，本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文，但由于OA文献来源多样且变更频繁，仍可能出现获取不到、文献不完整或与标题不符等情况，如果获取不到我们将提供退款服务。请知悉。

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
Naoharu Yoshitani;
展开▼
作者单位

展开▼
年度 2007
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. Normal and extreme aircraft accelerations and the effects on exposure to expiratory airborne contaminant inside commercial aircraft cabins A technical note in response to: "Are aircraft acceleration-induced body forces effective on contaminant dispersion in passenger aircraft cabins?" and "Airflow design and source control strategies for reducing airborne contaminant exposure in passenger aircraft cabins during the climb leg" (2019) in Sci. Technol. Built En. [J] . Elmaghraby Hossam A., Chiang Yi Wai, Aliabadi Amir A. Science and Technology for the Built Environment . 2020,第6a10期

机译：正常和极端的飞机加速度和对商用航空器舱内呼气空气污染物的影响的效果是响应的技术说明：“是飞机加速诱导的身体力量有效地对客机舱室中的污染物分散症状？” 和“用于减少乘客舱内的空气污染物暴露的气流设计和源控制策略”（2019年）SCI中的乘客舱。技术。建造en。
2. Nonlinear 3D path following control of a fixed-wing aircraft based on acceleration control [J] . Galffy A., Boeck M., Kugi A. Control Engineering Practice . 2019,第MAY期

机译：基于加速度控制的固定翼飞机非线性3D路径跟随控制
3. Nonlinear 3D path following control of a fixed-wing aircraft based on acceleration control [J] . Galffy A., Boeck M., Kugi A. Control Engineering Practice . 2019,第May期

机译：基于加速度控制的固定翼飞机控制下的非线性3D路径
4. FLIGHT TRAJECTORY CONTROL BASED ON REQUIRED ACCELERATION FOR FIXED-WING AIRCRAFT [C] . Naoharu Yoshitani Congress of the International Council of the Aeronautical Sciences;ICAS 2010 . 2010

机译：基于要求加速度的固定翼飞机飞行轨迹控制
5. Tail buffet alleviation of high performance twin tail aircraft using offset piezoceramic stack actuators and acceleration feedback control. [D] . Bayon de Noyer, Maxime P. 1999

机译：使用偏置压电陶瓷堆栈促动器和加速度反馈控制减轻高性能双尾飞机的尾巴自助餐。
6. A Personalized Diagnosis Method to Detect Faults in a Bearing Based on Acceleration Sensors and an FEM Simulation Driving Support Vector Machine [O] . Xiaoyang Liu, Haizhou Huang, Jiawei Xiang 2020

机译：基于加速度传感器和有限元模拟驱动支持向量机的轴承故障个性化诊断方法
7. A Heading and Flight-Path Angle Control of Aircraft Based on Required Acceleration Vector [O] . Naoharu Yoshitani 2004

机译：基于所需加速度向量的飞机标题和飞行路径角度控制
8. FLIGHT-PATH AND AIRSPEED CONTROL DURING LANDING APPROACH FOR POWERED-LIFT AIRCRAFT [R] . James A. Franklin, Robert C. Innis 1974

机译：动力升降机着陆方式中的航道和空中飞行控制

A Flight-Path Control of Aircraft Based on Required Acceleration Vector

著录项

引文网络

相似文献

相关主题

期刊订阅