Controllability ensuring during stages separation of launch vechicle low controller effectiveness of second stage

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Spacecraft Dynamics and Control
1Andronov, VA, 1Novikov, AV
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2001, 7 ;(Supplement1):082-088
https://doi.org/10.15407/knit2001.01s.082
Publication Language: Russian
Abstract: 
The problem of creation of necessary motion conditions for a phase of stages separation is formulated. Taking into account a received information about disturbances during launch vehicle (LV) flight, there are proposed two procedures of identification: wind action and main manufacturing disturbances. It is shown that problem of the LV controllability ensuring is solved as at the stages separation phase, either in qmax region.
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