小型无人直升机稳定杆建模与姿态系统设计

x对某小型无人直升机的稳定杆单独进行了建模,并着重分析了稳定杆在整个飞行控制系统中所起的作用以及它对姿态系统的影响。针对稳定杆所引起的姿态系统动态响应的峰值和弱阻尼,采取在控制策略中加入陷波器的方法进行补偿。仿真结果表明：陷波器消除了稳定杆所引起的峰值,提高了姿态系统的动态阻尼,姿态系统的性能得到了明显的优化,最后实现了姿态系统的自行稳定和按设定值变化,为小型无人直升机的姿态系统设计提供了工程设计方法。     

Microstructure and Mechanical Properties of Cross-rolled Ti50Ni47Fe3 Shape Memory Alloy

The microstructures, the phase transformation characteristics, and the mechanical properties of the Ti50Ni47Fe3 alloy in as-forged and as-cross-rolled states were investigated. It is found that, after cross-rolling, the phase transformation temperature （Ms） of the alloy decreases drastically and the grains get refined. Moreover, its yield strength and fracture strength after cross-rolling hit 540 MPa and 687 MPa respectively, up by about 200 MPa over those in as-forged state.     

ΔDsat,a QB50 CubeSat mission to study rarefied-gas drag modelling

A CubeSat mission to study the impact of flow incidence angle, surface material and surface roughness on gas–surface interactions on spacecraft in low Earth orbits has been designed. To accomplish this scientific goal the CubeSat deploys a variable geometry aerofoil capable of exposing different surfaces to the flow at different incident angles. By using the on-board GPS measurements and an orbit determination technique the drag experienced by the CubeSat can be estimated. The CubeSat has been designed to be part of the QB50 mission, and hence it carries a sensor that can take in-situ measurements of the atmosphere. This is then used to estimate the atmospheric density and hence to extract information on the drag coefficient. To minimise any bias present in the measurement chain a differential approach is used. Therefore no absolute drag coefficients are estimated, instead, ratios of drag coefficients are computed. This allows direct comparisons of the drag coefficients of different materials, different surface roughness or different incident angles. Simulations indicate that this CubeSat mission will be able to obtain drag coefficient ratios with an uncertainty level of less than 5%.     

Microstructure and Mechanical Properties of Cross-rolled Ti_(50)Ni_(47)Fe_3 Shape Memory Alloy

The microstructures, the phase transformation characteristics, and the mechanical properties of the Ti50Ni47Fe3 alloy in as-forged and as-cross-rolled states were investigated. It is found that, after cross-rolling, the phase transformation temperature (Ms) of the alloy decreases drastically and the grains get refined. Moreover, its yield strength and fracture strength after cross-rolling hit 540 MPa and 687 MPa respectively, up by about 200 MPa over those in as-forged state.     

上证50指数与其衍生品的波动特征及溢出效应

全球金融市场波动加剧,市场投资者规避风险需求增加,对具有风险规避功能的金融衍生品与其标的资产之间波动率相互影响的研究显得尤为重要.文章对上证50指数、上证50股指期货与50ETF三者之间的波动率溢出效应进行了实证研究,发现:上证50指数和上证50股指期货均对自身存在负向溢出,且三者收益率之间也存在均值外溢;上证50指数...     

On the planar inertial motion of a system of three coupled bodies

Numerous papers are devoted to studying the motion of a system (coupling) of two bodies in the Earth’s satellite orbit ([1–4] and others). The problem on the planar inertial motion of three bodies, coupled by a non-extensible weightless string having the form of an unfastened chain, is considered in the paper. Such a configuration can be represented, for example, by a system of two coupled spacecraft rotating around their common center of mass (in order to simulate the gravity force) in long-term space missions, when the third body (the lift) is located on a connecting cable. The bodies are considered to be the material points (particles).     

Some new applications of the generalized problem of two fixed centers

A generalized problem of two fixed centers and its limiting version is considered. New possible applications of this problem are obtained. Using a symmetric version of the problem, the external field of gravitation is approximated. The limiting version approximates the inner field.     

Navigation of a space bunch under conditions of its rotary motion

The properties of a tethered space system (bunch) in the mode of rotational motion are used in determination of the parameters of the location and orientation of the end vehicles of the bunch by the method with the simplest possible instrumental implementation.     

The motion of a particle in perturbed field of an attracting center

The integrable case of the perturbed two-body problem is considered. The perturbation is determined by the potential of a special form. The L-matrix is chosen in such a way that partial separation of variables should take place in regular coordinates. Integration of the equations of motion of the problem under consideration is made. The solutions are expressed through elliptic functions. The orbits for various cases are constructed. The results of numerical calculations are given.