DLR Portal
Home|Imprint|Sitemap|Contact |Deutsch
You are here: Home:Research:Space Robotics:Space Robotics Tools
Advanced Search
Robotics and Mechatronics Center
Institute of Robotics and Mechatronics
Institute of System Dynamics and Control
Institute for Optical Sensor Systems
News
Staff
Research
Rollin' Justin
Hand Arm System
Light-Weight Robots
Hands
Legged Robots
3D Modeller
Medical Robotics
Mechatronic devices
Biomimetic Robotics and Machine Learning
Telepresence & VR
Vision
Space Robotics
Ongoing Space Robotics Missions
Space Robotics Tools
Closed Space Robotics Missions
Flying Robots
Demonstrators
Flugzeug-Systemdynamik
Automotive
Railway Systems
Control Methods & Tools
Industrial Robot Control
Multikopter
Ausgründungen
Publications
Job offers
Downloadable Images
How to get to us
Kooperationen und Projekte
Space Robotics Tools
Back
Send article to a friendPrint

Motion Parameter Estimation for a Tumbling Satellite using a Model Based Approach



In this section a brief overview of the methodology considered for the motion parameter estimation for a tumbling satellite is described.

The problem consists in deriving a method for motion parameter estimation of a target by observation. This is intended for supporting a predictive simulation for the planning of a grasping sequence of the tumbling target. The position of the grasping point on the target as a function of time is unknown and must be derived from identification. The results of the identification must be accurate enough to allow for planning and execution within the limits of the robustness of a tracking controller.

The approaches being considered are the following:

  • Function approximation of the measured spacecraft states
  • Model based parameter identification of a spacecraft dynamic model

The latter point entails implementation of both linear as well as nonlinear least-squares methods, to account for non-linear inequality and normalization equality constraints.


Copyright © 2013 German Aerospace Center (DLR). All rights reserved.