000 00612 a2200241 4500
001 305058
020 _a
041 _aeng
080 _aLNASA CR - 3167 : 1979
245 _aA study of the application of singular perturbation theory
250 _a
260 _aWashington, D.C.
260 _bNational Aeronautics and Space Administration
260 _c1979
300 _a338 p.
300 _c
856 _u
490 _aLNASA CR - 3167 : 1979
700 _a
650 _a
650 _aSingular perturbation theory, Multiple scales, Continuation methods, F-4, Trajectory optimization
942 _cPP
942 _2UDC
999 _c253612
_d253612