Application of Hamilton Principle in the control of Tethered Satellite System Pendular Motion
Journal Title: INCAS BULLETIN - Year 2018, Vol 10, Issue 2
Abstract
The control of a tethered satellite system pendular motion is done by application of Hamiltonian equation of motion on a control design method known as planar H tracking. In this case, the reference motion is considered a natural planar motion. The control of the TSS is accomplished by using the inside plane control inputs as well as the outside plane control inputs. The designed control laws are able to drive the pendular motion to a natural planar trajectory with the required characteristics. The control inputs are analyzed using their magnitude ability. The numerical simulation results for each control inputs show that the inside of plane input not only has strong magnitude, but also effectively controls the pendular motion of the tethered satellite system.
Authors and Affiliations
Paul TIROP, Zhang JINGRUI
Keywords
Related Articles
- EP ID EP297134
- DOI 10.13111/2066-8201.2018.10.2.10
- Views 84
- Downloads 0
DESIGN & ANALYSIS TOOLS AND TECHNIQUES FOR AEROSPACE STRUCTURES IN A 3D VISUAL ENVIRONMENT
The main objective of this project is to develop a set of tools and to integrate techniques in a software package which is build on structure analysis applications based on Romanian engineers experience in designing and...
Test Rig Adaptation for WT Measurements for OR&TP Configurations
The need to test large models at maximum speed regimes close to 100 m/s, for which the aerodynamic forces and moments occurring on the model far exceed the measuring capability of the existing TEM external balance, made...
The mix of laws involved in the activity of the companies in the aerospace field
The life of companies, including the aerospace companies, depends on the business cycle. The paper presents the trends of law in ascending and descending period of the business cycle. A point of the paper is the separati...
Comprehensive study of endurance for IAR-99 Hawk
The paper presents some methods of on-ground and in-flight calibration for strain gauges, intended to the development of complex programs which analyze the endurance phenomena for aerospace structures, with direct applic...
A new solid particle erosion model for oriented fiber composite materials
The work describes a new model of erosion estimation equation which factors in both the impingement angle α and the fiber orientation angle β. Two examples of particular erosion equations are presented, for carbon fiber...