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Pulsed Thrust Method for Hover Formation FlyingA non-continuous thrust method for hover type formation flying has been developed. This method differs from a true hover which requires constant range and bearing from a reference vehicle. The new method uses a pulsed loop, or pogo, maneuver sequence that keeps the follower spacecraft within a defined box in a near hover situation. Equations are developed for the hover maintenance maneuvers. The constraints on the hover location, pulse interval, and maximum/minimum ranges are discussed.
Document ID
20030093749
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hope, Alan
(Naval Research Lab. United States)
Trask, Aaron
(Naval Research Lab. United States)
Date Acquired
August 21, 2013
Publication Date
April 15, 2003
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 2003 AAS/AIAA Astrodynamics Specialist Conference Meeting
Location: Big Sky, MT
Country: United States
Start Date: August 3, 2003
End Date: August 7, 2003
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Funding Number(s)
CONTRACT_GRANT: NDPR-S-65018-Y
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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