This paper proposes a compound control method for spacecraft multi-body separation which
is based on active disturbance rejection control (ADRC), aiming to address the problems of …

In this study, we investigate nonlinear dynamics of the autonomous separation deployment
maneuver for a space multi-rigid-body system with uncertain-but-bounded parameters by …

Stacked satellites have a promising application in aerospace engineering for the merits of
high launch efficiency and networking capability. As one of the key technical points …

广泛用于航天领域的单框架控制力矩陀螺, 具有力矩放大效应的优点, 其理论基础为有假设条件
的力矩放大原理. 本文不局限于这些假设, 不限定工况, 解析单框架控制力矩陀螺的输出特性 …

变体飞行器的气动弹性力学建模是当前先进飞行器设计的研究热点和难点. 然而传统的气动弹性
动力学建模方法对于具有结构参变特性的变体飞行器气动弹性力学研究存在建模效率低 …

橡胶材料因具有良好的抗震, 吸能作用, 在实际工程中应用广泛然而橡胶超弹性材料的碰撞属于
强非线性问题, 分析橡胶材料的接触碰撞和大变形问题对于提高装置的缓冲性能具有重要意义 …

堆叠卫星入轨后分离再重构是构建大型空间结构的有效手段之一. 使用自然坐标法建立堆叠卫星
系统的动力学方程, 具有方便处理卫星组装中固定约束的优点. 设置合适的堆叠卫星分离策略和 …

The parametric aeroelastic modeling of a morphing aircraft is a hot topic in the research field
of morphing aircraft design. However, the traditional non-parametric aeroelastic dynamic …

Space manipulators are typically installed on spacecraft using an emergency separation
device (ESD). In the event of a malfunction, the ESD ejects the manipulator from the …

The single-gimbal control moment gyroscope (SCMG), which is widely used in aerospace
field, has the advantage of torque amplification effect. It is based on the principle of torque …