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Sharma-Flight-Path Angle Control via Neuro-Adaptive Backstepping
Flight-Path Angle Control via
Neuro-Adaptive Backstepping
Manu Sharma? and David G. Ward?
Barron Associates, Inc.
1160 Pepsi Place Suite 300
Charlottesville, VA 22902
Abstract
A method of controlling flight-path angle via
neuro-adaptive backstepping is presented. Back-
stepping is used to circumvent the matching con-
dition, which can restrict feedback linearizing meth-
ods. Additionally, an on-line multilayer neural net-
work is used to provide robustness to aerodynamic
uncertainties in the plant model. The network also
simplifies the backstepping design because it obvi-
ates the need to construct a regressor, and does not
require an a-priori basis. Numerical simulation re-
sults show the viability of this approach.
Introduction
Various forms of nonlinear control have emerged
as enabling technologies for control of advanced
flight vehicles.1—3 Offering both increases in per-
formance as well as reduced development times by
dealing with the complete dynamics of the vehicle
rather than point designs, nonlinear control tools
provide a great deal of design flexibility. Feedback
linearization, in its various forms, is perhaps the
most commonly employed nonlinear control method
in this arena. However, the majority of the litera-
ture on feedback linearizing controllers treats some
combination of the aircraft’s angular rates (p, q, r),
aerodynamic angles (α,β), or Euler angles (φ, θ,ψ)
as the command variables. Using time-scale separa-
tion arguments, the plant dynamics are partitioned
into slow states and fast states, with the fast states
used as virtual controls for the slow.4 Another re-
striction on feedback linearization is the matching
condition, which requires that all parametric plant
uncertainties appear in the same equation of a state-
space representation as the control.5,6 This is of
significance in flight control where the plant aerody-
namics always contain some degree of uncertainty.
?Research Scientist, Member AIAA. sharma@
?Senior Research Scientist, Memb
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