NDLI: Analysis of disturbances in a leg of pitch-up maneuvering

Content Provider	Springer Nature Link
Author	Borisov, A. V. Ivav, R. K. Karpov, A. S. Sikharulidze, Yu. G.
Copyright Year	2006
Abstract	A complex model of disturbances for a leg of pitch-up maneuvering by a carrier aircraft in launching a launch vehicle was constructed. The model incorporates the atmospheric disturbances (wind gust, jet wind, and density variations), errors in the motion parameters at the point of beginning the maneuver, and the deviation of the initial mass of a launcher aircraft from the design mass. Such a model is required for a priori estimation of the operational requirements (in normal load factor and attack angle), as well as for determination of possible initial errors in the motion of the launch vehicle due to the air launch. We present majority estimates of errors for the most unfavorable combination of disturbances and the results of statistical analysis for the disturbed-motion trajectories by the Monte Carlo method.
Starting Page	497
Ending Page	507
Page Count	11
File Format	PDF
ISSN	10642307
Journal	Journal of Computer and Systems Sciences International
Volume Number	45
Issue Number	3
e-ISSN	15556530
Language	English
Publisher	Nauka/Interperiodica
Publisher Date	2006-01-01
Publisher Place	Moscow
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Control Engineering
Content Type	Text
Resource Type	Article
Subject	Applied Mathematics Theoretical Computer Science Computer Networks and Communications Control and Systems Engineering Information Systems Computer Vision and Pattern Recognition Software

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