NDLI: On the feedback linearization control for hypersonic flight vehicle analogy X20

Content Provider	IEEE Xplore Digital Library
Author	Gong Yulian Meng Bin
Copyright Year	2014
Description	Author affiliation: Sci. & Technol. on Space Intell. Control Lab., Beijing Inst. of Control Eng., Beijing, China (Gong Yulian; Meng Bin)
Abstract	In this paper, we consider the control problem of the hypersonic flight vehicle analogy X20. Through a careful analysis of the relationship between the aerodynamic coefficients and their independent variables of height, Mach number, attack angle, sideslip angle and rudder angel, we fit the aerodynamic coefficients according to the independent variables and give their analytic expressions. And we establish the affine nonlinear control model of analogy X20, which is proved the input-output linearization. On the basis, we design the feedback linearization control law. When there being the uncertainties of aero density, aerodynamic moment coefficients and inertia, the simulations are performed for the original dynamics, which include the earth rotation and whose aerodynamic data come from the aerodynamic data table directly. The simulation results indicate that the resulting control law ensures the control targets and has strong robustness.
Starting Page	934
Ending Page	938
File Size	1751948
Page Count	5
File Format	PDF
ISBN	9781479937073
e-ISBN	9781479937080
DOI	10.1109/CCDC.2014.6852297
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-05-31
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Space vehicles Control engineering Analogy X20 Space technology Aerospace electronics Aerodynamics Aerodynamic coefficient fitting Hypersonic flight vehicles Feedback linearization Intelligent control Control model
Content Type	Text
Resource Type	Article

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