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SCIENTIFIC AND TECHNICAL AEROSPACE REPORTS

A Biweekly Publication of the National Aeronautics and Space Administration
VOLUME 43, ISSUE 16 - AUGUST 12, 2005

NASA STAR REPORTS: 08/12/05
Astronautics

12 Astronautics (General)

13 Astrodynamics

14 Ground Support Systems and Facilities

15 Launch Vehicles and Launch Operations

16 Space Transportation and Safety

17 Space Communications, Spacecraft Communications, Command and Tracking

18 Spacecraft Design, Testing and Performance

20 Spacecraft Propulsion and Power

13 ASTRODYNAMICS
Includes powered and free flight trajectories; orbital and launching dynamics.


20050196278 Air Force Inst. of Tech., Wright-Patterson AFB, OH USA

A Numerical Analysis for Passive Attitude Stabilization Using a Tethered Balloon on a Gravity Gradient Satellite

Maramba, Ernest M.; Mar. 2005; 120 pp.; In English; Original contains color illustrations Report No.(s): AD-A435263; AFIT/GA/ENY/05-M07; No Copyright; Avail: Defense Technical Information Center (DTIC)


This research effort analyzes the fundamental dynamics governing a satellite with a gravity gradient boom and a tethered balloon. Satellites that use gravity gradient booms for passive attitude control are characterized by undamped pitch oscillations and no roll control. The tethered balloon acts as a high drag device that accounts for the most drag on the satellite system. By attaching a drag device, the system resists rolling movements while also damping oscillations. This could potentially be a cost effective method for increasing satellite stabilization. The goal of this research is to model the dynamics and determine the feasibility of a gravity gradient stabilized satellite with an attached balloon. A simulation written in Matlab analyzes the behavior of such a satellite. The research is limited to circular orbits around a spherical Earth and includes only in-plane motion for each mass. Stable ranges for certain tether characteristics are found for three different satellites. DTIC

Artificial Satellites; Attitude (Inclination); Attitude Control; Attitude Stability; Gravity Gradient Satellites; Numerical Analysis; Tethered Balloons


Source: NASA.


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