Yatin Chaudhary 2026-04-13T12:33:18+00:00 Writer LibreOffice 7.3 engines={image=false textcolor=true vector=false text=true} tetml={filename={D:\drim\repository\projects\drim_50_0\metadata\6\5\6560bc6974711b6dc29784e8009fc655\6560bc6974711b6dc29784e8009fc655.para.xml} elements={annotations=false bookmarks=false destinations=false fields=false javascripts=false} } granularity=word tetml={elements={line} glyphdetails={all}} contentanalysis={punctuationbreaks=false dehyphenate=false shadowdetect=false} layoutanalysis={tabledetect=0 layoutdetect=3} structureanalysis={list=true} Enrich E n r i c h Table T a b l e ROBs R O B s Test T e s t File F i l e Requirement R e q u i r e m e n t ID I D EXTID-216 E X T I D - 2 1 6 EXTID-217 E X T I D - 2 1 7 EXTID-218 E X T I D - 2 1 8 EXTID-219 E X T I D - 2 1 9 Text T e x t Information I n f o r m a t i o n of o f Requirement R e q u i r e m e n t ID I D In I n case c a s e of o f an a n error e r r o r of o f the t h e system s y s t e m coolant c o o l a n t temperature t e m p e r a t u r e sensor, s e n s o r , there t h e r e shall s h a l l be b e a a limp l i m p home h o m e value v a l u e as a s close c l o s e as a s possible p o s s i b l e to t o the t h e real r e a l system s y s t e m temperature t e m p e r a t u r e (e.g. ( e . g . using u s i n g other o t h e r temperature t e m p e r a t u r e sensors s e n s o r s or o r limp l i m p home h o m e model). m o d e l ) . In I n case c a s e of o f existing e x i s t i n g external e x t e r n a l heater h e a t e r the t h e system s y s t e m coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l be b e adapted a d a p t e d to t o the t h e influence i n fl u e n c e of o f the t h e external e x t e r n a l heater, h e a t e r , to t o provide p r o v i d e the t h e real r e a l engine e n g i n e temperature t e m p e r a t u r e to t o the t h e system s y s t e m to t o ensure e n s u r e a a robust r o b u s t engine e n g i n e start. s t a r t . In I n case c a s e of o f an a n unsuccessful u n s u c c e s s f u l engine e n g i n e start s t a r t it i t is i s assumed a s s u m e d that t h a t the t h e temperature t e m p e r a t u r e sensor s e n s o r could c o u l d be b e defect. d e f e c t . Therefore T h e r e f o r e a a substitute s u b s t i t u t e value v a l u e (e.g. ( e . g . TAM, T A M , TIA, T I A , modeled m o d e l e d temperature, t e m p e r a t u r e , ...) . . . ) shall s h a l l be b e used u s e d for f o r the t h e system s y s t e m coolant c o o l a n t temperature. t e m p e r a t u r e . The T h e final fi n a l SW S W value v a l u e coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l represent r e p r e s e n t correct c o r r e c t value v a l u e of o f coolant c o o l a n t temperature t e m p e r a t u r e (after ( a f t e r all a l l diagnosis d i a g n o s i s and a n d plausibility p l a u s i b i l i t y checks) c h e c k s ) Text T e x t Information I n f o r m a t i o n of o f Requirement R e q u i r e m e n t ID I D In I n case c a s e of o f an a n error e r r o r of o f the t h e system s y s t e m coolant c o o l a n t temperature t e m p e r a t u r e sensor, s e n s o r , there t h e r e shall s h a l l be b e a a limp l i m p home h o m e value v a l u e as a s close c l o s e as a s possible p o s s i b l e to t o the t h e real r e a l system s y s t e m temperature t e m p e r a t u r e (e.g. ( e . g . using u s i n g other o t h e r temperature t e m p e r a t u r e sensors s e n s o r s or o r limp l i m p home h o m e model). m o d e l ) . In I n case c a s e of o f existing e x i s t i n g external e x t e r n a l heater h e a t e r the t h e system s y s t e m coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l be b e adapted a d a p t e d to t o the t h e influence i n fl u e n c e of o f the t h e external e x t e r n a l heater, h e a t e r , to t o provide p r o v i d e the t h e real r e a l engine e n g i n e temperature t e m p e r a t u r e to t o the t h e system s y s t e m to t o ensure e n s u r e a a robust r o b u s t engine e n g i n e start. s t a r t . In I n case c a s e of o f an a n unsuccessful u n s u c c e s s f u l engine e n g i n e start s t a r t it i t is i s assumed a s s u m e d that t h a t the t h e temperature t e m p e r a t u r e sensor s e n s o r could c o u l d be b e defect. d e f e c t . Therefore T h e r e f o r e a a substitute s u b s t i t u t e value v a l u e (e.g. ( e . g . TAM, T A M , TIA, T I A , modeled m o d e l e d temperature, t e m p e r a t u r e , ...) . . . ) shall s h a l l be b e used u s e d for f o r the t h e system s y s t e m coolant c o o l a n t temperature. t e m p e r a t u r e . The T h e final fi n a l SW S W value v a l u e coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l represent r e p r e s e n t correct c o r r e c t value v a l u e of o f coolant c o o l a n t temperature t e m p e r a t u r e (after ( a f t e r all a l l diagnosis d i a g n o s i s and a n d plausibility p l a u s i b i l i t y checks) c h e c k s ) granularity=word tetml={elements={line} glyphdetails={all}} contentanalysis={punctuationbreaks=false dehyphenate=false shadowdetect=false} layoutanalysis={tabledetect=0 layoutdetect=3} structureanalysis={list=true} Requirement R e q u i r e m e n t ID I D Text T e x t Information I n f o r m a t i o n of o f Requirement R e q u i r e m e n t ID I D EXTID-226 E X T I D - 2 2 6 EXTID-227 E X T I D - 2 2 7 EXTID-228 E X T I D - 2 2 8 EXTID-229 E X T I D - 2 2 9 The T h e system s y s t e m shall s h a l l take t a k e conditions c o n d i t i o n s into i n t o account a c c o u n t where w h e r e the t h e combustion c o m b u s t i o n engine e n g i n e is i s stopped s t o p p e d and a n d the t h e vehicle v e h i c l e is i s moving m o v i n g e.g. e . g . engine e n g i n e off o ff coasting c o a s t i n g or o r electric e l e c t r i c driving. d r i v i n g . The T h e respective r e s p e c t i v e temperature t e m p e r a t u r e models m o d e l s must m u s t be b e adapted. a d a p t e d . The T h e calculation c a l c u l a t i o n of o f the t h e coolant c o o l a n t temperature t e m p e r a t u r e should s h o u l d only o n l y take t a k e into i n t o account a c c o u n t the t h e combustion c o m b u s t i o n engine e n g i n e load. l o a d . Any A n y support s u p p o r t by b y electric e l e c t r i c machine(s) m a c h i n e ( s ) shall s h a l l not n o t lead l e a d to t o an a n incorrect i n c o r r e c t calculation c a l c u l a t i o n of o f the t h e coolant c o o l a n t temperature. t e m p e r a t u r e . Frequency F r e q u e n c y range r a n g e of o f the t h e antenna a n t e n n a should s h o u l d be b e 50 5 0 MHz-6 M H z - 6 GHz. G H z . In I n case c a s e of o f existing e x i s t i n g external e x t e r n a l heater h e a t e r the t h e system s y s t e m coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l be b e adapted a d a p t e d to t o the t h e influence i n fl u e n c e of o f the t h e external e x t e r n a l heater, h e a t e r , to t o provide p r o v i d e the t h e real r e a l engine e n g i n e temperature t e m p e r a t u r e to t o the t h e system s y s t e m to t o ensure e n s u r e a a robust r o b u s t engine e n g i n e start. s t a r t . Eccentricity E c c e n t r i c i t y of o f the t h e antenna a n t e n n a should s h o u l d be b e ≤±5 ≤ ± 5 dB. d B . In I n case c a s e of o f an a n unsuccessful u n s u c c e s s f u l engine e n g i n e start s t a r t it i t is i s assumed a s s u m e d that t h a t the t h e temperature t e m p e r a t u r e sensor s e n s o r could c o u l d be b e defect. d e f e c t . Therefore T h e r e f o r e a a substitute s u b s t i t u t e value v a l u e (e.g. ( e . g . TAM, T A M , TIA, T I A , modeled m o d e l e d temperature, t e m p e r a t u r e , ...) . . . ) shall s h a l l be b e used u s e d for f o r the t h e system s y s t e m coolant c o o l a n t temperature. t e m p e r a t u r e . Charakteristik C h a r a k t e r i s t i k of o f the t h e antenna a n t e n n a should s h o u l d be b e omnidirectional. o m n i d i r e c t i o n a l . The T h e final fi n a l SW S W value v a l u e coolant c o o l a n t temperature t e m p e r a t u r e shall s h a l l represent r e p r e s e n t correct c o r r e c t value v a l u e of o f coolant c o o l a n t temperature t e m p e r a t u r e (after ( a f t e r all a l l diagnosis d i a g n o s i s and a n d plausibility p l a u s i b i l i t y checks). c h e c k s ) . Weight W e i g h t of o f the t h e antenna a n t e n n a should s h o u l d be b e Max M a x 20 2 0 kg. k g . 0.06 0.28 0.38 0.00 0.00 0.00