1.
Research on the Method of Aircraft Pose Surveying from Image Sequences Obtained by Photoelectric Theodolite;
基于光电经纬仪影像的飞机姿态测量方法研究
2.
Measurement of aircraft attitude by spatial cosine relationship in single-station and planes to intersection in multi-station of electro-optical theodolite
光电经纬仪单站空间余弦及多站面面交汇的飞机姿态测量
3.
CALCULATION FOR ATTITUDE ANGLES OF AN ALL ATTITUDE AEROPLANE STRAPDOWN SYSTEM
![点击朗读](/dictall/images/read.gif)
全姿态飞机捷联式系统姿态角的计算
4.
LARGE ANGLE ATTITUDE MANEUVERS AND CONTROLS OF GYROSTAT SPACECRAFT
![点击朗读](/dictall/images/read.gif)
陀螺体飞行器大角度姿态机动与控制
5.
Research of the Robust Attitude Control for a Subminiature Unmanned Helicopter
![点击朗读](/dictall/images/read.gif)
超小型无人直升机飞行姿态的鲁棒控制研究
6.
Muzzle Attachment's Influence on the Flying Bullets Attitude of Double-autogun
![点击朗读](/dictall/images/read.gif)
膛口装置对双联自动机弹丸飞行姿态影响研究
7.
Fast Pose Estimation Method for Flight Vehicles Based on Computer Vision
![点击朗读](/dictall/images/read.gif)
基于计算机视觉的飞行器姿态快速估计方法
8.
Then perform 5/8 loop, helicopter should be inverted on a 45 degree down line.
![点击朗读](/dictall/images/read.gif)
执行5/8内浸斗,使直升机成为倒飞的姿态,机头向下45°。
9.
The helicopter should be inverted as it passes in front of the pilot.
![点击朗读](/dictall/images/read.gif)
当直升机到达操控者的正前方时,机体刚好成为倒飞的姿态。
10.
A Mathematical Model of Unmanned Tiltrotor Aircraft and Research on Attitude Control System Design;
无人倾转旋翼机飞行力学建模与姿态控制技术研究
11.
The aircraft should remain in a hover only as long as is necessary to employ ordnance. Once complete, the pilot should resume normal flight.
飞机只应在尽可能短的必要的开火时间里悬停,完成攻击后立即回复平常的飞行姿态。
12.
attitude control propulsion motor
![点击朗读](/dictall/images/read.gif)
姿态控制推进电动机
13.
Research on Attitude Control about Aerospace Vehicle Based on Multi-Agent;
![点击朗读](/dictall/images/read.gif)
基于多Agent的空天飞行器的姿态控制
14.
Relative Attitude Dynamics and Control in Satellite Formation Flying
![点击朗读](/dictall/images/read.gif)
卫星编队飞行相对姿态动力学与控制
15.
Adaptive Attitude Coordination Control of Formation Flying Satellite
![点击朗读](/dictall/images/read.gif)
编队飞行卫星的自适应姿态协同控制
16.
An Aircraft Attitude Indication System Based on MEMS
![点击朗读](/dictall/images/read.gif)
基于MEMS传感器的飞行姿态指示系统
17.
Research on Satellite Attitude Control Problem in the State of Energy Storage & Attitude Control Double-duty Flywheel Energy Feedback;
卫星储能/姿控两用飞轮在能量回馈状态下的姿态控制问题研究
18.
The Chaotic Attitude Control in the Large Angle Attitude Maneuver of Liquid-Filled Flexible Spacecraft
柔性充液航天器姿态转换机动及混沌姿态控制