Advances in aerospace systems dynamics and control systems. by Cornelius T. Leondes

By Cornelius T. Leondes

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Extra resources for Advances in aerospace systems dynamics and control systems. Part 3 of 3

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I n S e c t i o n IV, t h e m e a s u r e d r e s p o n s e c h a r a c t e r i s t i c s of a n o p e r a t o r is c o m p a r e d w i t h t h e s i m u l a t e d b e h a v i o r of t h e m o d e l . A t i m e - v a r y i n g s c e n e w a s p r e s e n t e d t o a s u b j e c t w h o w a s a s k e d t o i n d i c a t e a level of c o n f i d e n c e t h a t a t a r g e t (a t a n k ) w a s w i t h i n t h e field of view. T h i s r e s p o n s e a l o n g w i t h t h e a c t u a l l o c a t i o n s of t a r g e t s , d e c o y s , a n d o p e n r e g i o n s w a s r e c o r d e d .

D e t a i l is selectively r e m o v e d f r o m t h e d e t a i l e d s i m u l a t i o n t o maximize simplicity while m a i n t a i n i n g accuracy. This process requires a great d e a l of j u d g m e n t a n d is n o t s t r a i g h t f o r w a r d o r s y s t e m a t i c . I n a d d i t i o n , simplified m o d e l p e r f o r m a n c e is n o t easily p r e d i c t e d . A simplified c o m p o n e n t m o d e l r e l a t e s n a t u r a l l y t o t h e p h y s i c s of t h e a c t u a l e n g i n e a n d , t h e r e f o r e , is r e a d i l y u n d e r s t a n d a b l e .

T h r o t t l e t r a n s i e n t s w e r e p e r f o r m e d b y i n d u c i n g t h e failures b e f o r e a n d d u r i n g t h e t h r o t t l e m o v e m e n t . T h e s e n s o r s failed d u r i n g t h e flight test i n c l u d e d t h e c o m p r e s s o r inlet v a r i a b l e g e o m e t r y s e n s o r , P S 2 , P B , a n d F T I T . M o s t failures w e r e d e t e c t e d a n d a c c o m m o d a t e d . H o w e v e r , a r e c r e a t i o n of a b r o k e n line ( h a r d ) P B failure w e n t u n d e t e c t e d .

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