An impending demand for exploring the small bodies such as the comets and t
he asteroids envisioned the Japanese MUSES-C mission to the near Earth aste
roid Nereus, An autonomous optical guidance and navigation strategy around
the asteroid is discussed in this paper. Four major new schemes are dealt w
ith hers: They are (1) Aligned intercept guidance, (2) Strategic building o
f the flight phases, (3) Image processing of line-of-sight shift informatio
n instead of characteristic point tracking, and (4) Stability and accuracy
analysis associated with the guidance and navigation strategies developed h
ere. Some comprehensive numerical illustrations are also given to support t
hem. 1999 Elsevier Science Ltd. All rights reserved.