<DOC>
<DOCNO>
532
</DOCNO>
<TITLE>
pitch-yaw stability of a missile oscillating in roll
via the second method of lyapunov .
</TITLE>
<AUTHOR>
parks,p.c.
</AUTHOR>
<BIBLIO>
j. ae. scs. 29, 1962, 874.
</BIBLIO>
<TEXT>
the stability theory of a. m. lyapunov, a popular topic in
the u.s.s.r., is receiving increasing attention elsewhere .
this note describes lyapunov's /second method/ very briefly
and applies it to an aeronautical stability problem .
</TEXT>
</DOC>
