[1] OEHRLI R R.Effect of gun pulse on helicopter attitudes[R].[S.l.]:[s.n.],1976:1-38.
[6] TIWARI P M,JANARDHANAN S,NABI M U.Attitude control using higher order sliding mode[J].Aerospace Science and Technology,2016,54:108-113.
[7] DOMAN'SKI P D.Performance assessment of predictive control-a survey[J].Algorithms,2020,13(4):97-102.
[8] BECHLIOULIS C P,ROVITHAKIS G A.Robust adaptive control of feedback linearizable MIMO nonlinear systems with prescribed performance[J].IEEE Transactions on Automatic Control,2008,53(9):2090-2099.
[11] ZHANG Y,WANG S H,CHANG B,et al.Adaptive constrained backstepping controller with prescribed performance methodology for carrier-based UAV[J].Aerospace Science and Technology,2019,92:55-65.
[12] TAN J,GUO S J.Backstepping control with fixed-time prescribed performance for fixed wing UAV under model uncertainties and external disturbances[J].International Journal of Control,2020,93:1-18.
[13] HILBERT K B.A mathematical model of the UH-60 helicopter[R].Washington D.C.:NASA,1984.
[14] HOWLETT J J.UH-60A black hawk engineering simulation program.volume 1:mathematical model[R].Washington D.C.:NASA,1981.