NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A review of some exact solutions to the planar equations of motion of a thrusting spacecraftWith the complexities in computing optimal low thrust trajectories, easily-computed, good sub-optimal trajectories provide both a practical alternative for mission designers and a starting point for optimisation. The present paper collects in one place for easy reference and comparison several exact solutions that have been obtained in the literature over the last few decades: the logarithmic spiral, Pinkham's variant thereof, Forbes spiral, the exponential sinusoid, the case of constant radial thrust, Markopoulos's Keplerian thrust arcs, Lawden's spiral, and the analogous Bishop and Azimov spiral.
Document ID
20060029580
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Petropoulos, A. E.
Sims, J. A.
Date Acquired
August 23, 2013
Publication Date
June 18, 2002
Subject Category
Astrodynamics
Distribution Limits
Public
Copyright
Other
Keywords
low-thrust trajectories electric propulsion solar sail

Available Downloads

There are no available downloads for this record.
No Preview Available