NASA NTRS · 19920019492
Fuel optimal maneuver: Experimental testbeds
Abstract
The objective of this paper is to conduct experiments in fuel optimal propulsive maneuvers of flexible spacecraft in order to verify and extend recently developed theory and apply it to various classes of spacecraft. Topics covered in viewgraph format include: impulse damping control by experimental verification; impulse damping of the SCOLE reflector and mast; fuel optimal control of rotating flexible beam; fuel optimal aerobrake maneuvers.
Keep this discovery
Explore connections, maps & timelines
Meyer, John L.. 1992-07-01. Fuel optimal maneuver: Experimental testbeds. https://ntrs.nasa.gov/citations/19920019492
Cite the original work for its findings. Save a collection to share your selection of sources.