The coupling dynamics of the pitching of spacecraft, the sloshing of liquid fuel and the vibration of elastic appendages are investigated.
该文考虑了带弹性帆板与液体燃料的航天器做俯仰运动时刚-液-弹之间的相互耦合作用,采用已推导的刚-液-弹耦合系统非线性动力学方程组,应用多尺度法解析分析耦合系统的液体一阶主共振,利用奇异性理论对分岔方程进行分析,得到多种分岔模式,随后根据该文研究的耦合系统物理系数范围,确定只存在滞后点分岔,表现为幅频曲线软、硬特性的转换现象。
The coupled dynamics of the pitching of a spacecraft,the sloshing of liquid fuel and the vibration of elastic appendages is investigated.
考虑了带弹性帆板与液体燃料的航天器做俯仰运动时刚-液-弹之间的相互耦合作用,采用已推导的刚-液-弹耦合系统非线性动力学方程组,应用多尺度法对耦合系统液体一阶主共振的非线性动力学特性进行解析分析,发现了幅频曲线软、硬特性随液深发生转换的现象,发生转换时的临界液深值大小与液体燃料在航天器中的位置、航天器与弹性帆板的转动惯量相对于液体燃料密度的比值均有关,并通过与数值模拟比较,验证了解析分析的正确性。
The effects of fuel position on the attitude of spacecraft with elastic appendages were studied under the condition that the fuel sloshes violently and assuming that the coupling system pitches round the mass center of the whole system.
假设耦合系统绕系统质心做俯仰运动,首先采用已推导的刚-液-弹耦合系统俯仰运动非线性动力学方程组,得到系统固有频率,给出固有频率简单近似解析表达式,分析充液箱位置对系统各阶固有频率的影响。
Investigation of dynamic test technology for a model pitching oscillation with large amplitude in high speed wind tunnels;
高速风洞大振幅俯仰动态试验技术研究
A pitching test set-up, used in the unsteady wind tunnel at Nanjing University of Aeronautics & Astronautics, is developed to study the effect of rapid changes on both the free stream velocity and the angle of attack.
在南京航空航天大学已建成的国内首座非定常风洞内,研制了一套单自由度俯仰振荡实验装置,设计开发了一套对模型姿态和来流风速进行联合控制的软件。
We have an empirical knowledge that the rear suspension should have a higher spring rate than front one, in order to reduce pitching motion.
为了减少俯仰运动,后悬架应该比前悬架有较高的弹簧刚度。
The coupling dynamics of the pitching of spacecraft,the sloshing of liquid fuel and the vibration of elastic appendages are investigated in this paper.
采用已推导的俯仰运动矩形贮箱受控刚-液-弹耦合系统在外力矩作用下的耦合动力学模型,在刚体上加入控制项,详细分析了系统固有频率的精确解与近似解。
In the case of pitch excitation,the modified potential function and wave height function were introduced to describe the moving boundary of fluid.
首先建立了俯仰运动矩形贮箱刚-液-弹耦合系统在外力矩作用下的耦合动力学模型,给出满足边界条件的速度势函数和液面波高的级数表达式,采用伽辽金法离散,将动力学模型转化为常微分方程组,得到刚-液-弹耦合系统的固有频率,给出简单的近似表达式,分析了转动中心距静液面不同位置时刚-液-弹耦合系统各阶固有频率的变化规律,系统转动中心距静液面较近时,耦合后液体反对称模态和刚体的固有频率对比耦合前减小,较远时则增大,最后进行数值验证,比较分析了液体和弹性体对刚体姿态的影响。
Elevation-azimuth type antenna pedestal
俯仰-方位型天线座
gyroscopic bank and pitch indicator
陀螺倾斜及俯仰指示器
luffing winch motor
俯仰式起重机电动机
elevation servo power amplifier
俯仰伺服功率放大器
The comet passed by in the twinkling of an eye.
俯仰之间, 流星闪过。
The Perception of Nature and the Viewpoint of Universe;
仰观俯察的自然意识与俯仰自得的宇宙视角
His mood inclined to melancholy and retrospection.
他不禁感慨系之，俯仰今昔起来。
Vertical axis type elevation-azimuth antenna pedestal
立轴式俯仰-方位型天线座
Rotary table type elevation-azimuth antenna pedestal
转台式俯仰-方位型天线座
Roller raceway type elevation-azimuth antenna pedestal
轮轨式俯仰-方位型天线座
gantry crane with level luffing crane
带俯仰式吊车的龙门起重机
The Emergence of Confucianism and Taoism about Shan Tao;
心存事外,与时俯仰——山涛玄儒兼治研究
Study of Parameter tuning in Human Motion Perception System Based on the Electro-Motive
电动人感系统俯仰通道参数整定研究
Numerical Study of Pitching Dynamic Characteristic for Hypersonic Missile
高超声速弹头俯仰动态特性数值研究
The Control System of Pitching Collimation Based on Rotary Transformer
基于旋转变压器的俯仰瞄准控制系统
Pitch angular velocity estimate based on Kalman Filtering
基于Kalman滤波的俯仰角速度估计
Independent pitch and yaw of the two birds produce noise.
两只吊舱的独立俯仰和偏航均会产生噪声。
pitching headlong with a rolling or twisting movement.
伴随一个旋转或扭曲的运动头向前俯仰的。