By Agneta Balint (Ed)
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Introduce a virtual control α 1 and an error state z , and rewrite the current state equation in terms of these; 2. choose a CLF for the system, treating it as a final stage; 3) choose an equation for the virtual control that makes the CLF stabilizable. The CLF is augmented at subsequent steps to reflect the presence of new virtual states, but the same three stages are followed at each step. Hence, backstepping is a recursive design procedure. , 1991), which achieves boundedness of the closedloop states and convergence of the tracking error to zero.
The responses at the two other flight conditions are virtually the same, although less thrust is needed due to the lower altitude of flight condition 2 and the lower airspeed of flight condition 3. The other control surfaces are also more efficient. This is illustrated in Tables 2–4, in which the mean absolute values (MAVs) of the outer-loop tracking errors, control-surface deflections, and thrust can be found. Plots of the parameter-estimation errors are not included. , 2007, Page and Steinberg, 1999).
28] Barrett, R. , "Modeling, Design and Testing of a Barrel-Launched Adaptive Munition," proceedings of the 4" Annual SPIE Symposium on Smart Structures and Materials, San Diego, CA, 3-6 March 1997. , Niceville, Florida, 1993.  Hertlein, Robert and Mark Miner, “Extended Range Guided Munition (ERGM) Safe and Arm Device and Height-of-Burst Sensor,” paper presented at the NDIA Fuse Conference, 9 April 2993, New Orleans, LA. pdf  Pike, J. org, Alexandria, Virginia, October, 2002. htm). , “M732A2 Proximity Fuse and M782 Multi-Option Fuse for Artillery (MOFA) Data Sheets,” published by Alliant Techsystems, Inc.
Advances in Flight Control Systems by Agneta Balint (Ed)