... WσΨσ( 24) ˆG= G∗+ WδΨδ(25)58 Advances in Flight Control Systems Advances in Flight Control Systems 50 7. References Clough, B. T. (2005), “Unmanned Aerial Vehicles: Autonomous Control ... an indirect adaptivelaw which updates the model inversion controller; and moreoverˆG is ensured to be invertibleby verifying its matrix conditioning number.56 Advances in Flight Control Systems The ... 20 30 40 −0 .4 −0.200.20 .4 t, secr, deg/sec 0 10 20 30 40 −0 .4 −0.200.20 .4 0.6t, secr, deg/sec 0 10 20 30 40 −0 .4 −0.200.20 .4 t, secr, deg/sec 0 10 20 30 40 −0 .4 −0.200.20 .4 0.6t,...