In order to simulate the behavior of a space multibody system, the paper shows the possibility of shifting from a Newton Euler (NE) multibody approach to an Euler Lagrange (EL) formulation of the equations of motion. The NE is convenient to understand and to write down the mechanics equations of the system, but the EL equations of motion have a minimum mathematical complexity and a minimum number of equations in a minimum number of variables. The proposed procedure also allows to turn back to the NE formulation to calculate the reaction forces and torques among the bodies. The overall revised hybrid formulation, built by mixing both NE and EL approaches, is applied for simulating the deploying phase of spacecraft solar panels
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
In order to simulate the behavior of a space multibody system, the paper shows the possibility of sh...
In the past the deployment of space structures has widely been analysed by using multibody formulati...
Multibody dynamics for space applications is dictated by space environment such as space-varying gra...
The paper describes the motion of a multibody in space environment: by space environment we mean spa...
The need to model very complex spacecraft has induced many researchers to develop different methodol...
A relatively general formulation for the governing equations of motion, applicable to a large class ...
The Magnetospheric MultiScale (MMS) mission employs a formation of spinning spacecraft with several ...
We present here a method and some tools developed to build linear models of multi-body systems for s...
The equation of motion of a multibody system, described here as a chain of rigid bars and revolute j...
In this paper, a new approach to the modelling of the deployment dynamics of a flexible multi-body s...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
In order to simulate the behavior of a space multibody system, the paper shows the possibility of sh...
In the past the deployment of space structures has widely been analysed by using multibody formulati...
Multibody dynamics for space applications is dictated by space environment such as space-varying gra...
The paper describes the motion of a multibody in space environment: by space environment we mean spa...
The need to model very complex spacecraft has induced many researchers to develop different methodol...
A relatively general formulation for the governing equations of motion, applicable to a large class ...
The Magnetospheric MultiScale (MMS) mission employs a formation of spinning spacecraft with several ...
We present here a method and some tools developed to build linear models of multi-body systems for s...
The equation of motion of a multibody system, described here as a chain of rigid bars and revolute j...
In this paper, a new approach to the modelling of the deployment dynamics of a flexible multi-body s...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...
Recently, the interest of the space agencies in missions involving the soft-landing of a spacecraft...