By Agneta Balint (Ed)
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Extra resources for Advances in Flight Control Systems
Future studies will focus on the actual trajectory generation and the extension to formation-flying control. Appendix constraint adaptive backstepping Backstepping  is a systematic, Lyapunov-based method for nonlinear control design, which can be applied to nonlinear systems that can be transformed into lower-triangular form, such as the system of Eq. 1) The name “backstepping” refers to the recursive nature of the control law design procedure. Using the backstepping procedure, a control law is recursively constructed, along with a control Lyapunov function (CLF) to guarantee global stability.
5 (δ a ± 10π / 180 ) ]. Figure 5 shows the response at flight condition 3 with the aileron locked at -10 deg. Except for some small oscillations in the response of roll rate p, there is no real change in performance visible; this is confirmed by the numbers of Table 4. However, from Tables 2 and 3 we observe that aileron and rudder deflections become larger with both locked aileron failure cases, whereas tracking performance hardly declines. 3 Manoeuvre 2: reconnaissance The second maneuver, called reconnaissance and surveillance, involves turns in both directions and altitude changes, but airspeed is kept constant.
F-49620-93-C-0063, USAF Wright Laboratory Flight Vehicles Branch, WL/MNAV August, 1995. , and Stutts, J. "Barrel-Launched Adaptive Munition BLAM Experimental Round Research," final report for USAF contract no. F-49620-C-0063, USAF Wright Laboratory Flight Vehicles Branch, WL/MNAV February, 1997. , "Cone Aerodynamics Test", Aeroballistic Research Facility Ballistic Spark Range Technical Report, USAF Wright Laboratory Flight Vehicles Branch, WL/MNAV June 1996.  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.
Advances in Flight Control Systems by Agneta Balint (Ed)