Abstract

Areas of s t ab i l i ty a r e der ived for miss i l e c o n t r o l s y s t e m s w i t h l i nea r a n d n o n l i n e a r servo c o m p o n e n t s . M e t h o d s a re shown t o a d a p t s ignal p h a s e sh i f t ing n e t w o r k s t o t h e p r o p er t ies of t h e miss i le a n d a selected servo s y s t e m . T h e i n ves t iga t ions a r e ex tended t o miss i le m o t i o n s a r o u n d i t s c en t e r of gravi ty a n d a b o u t a p rescr ibed l ine of flight.

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