Adaptive Fuzzy Sliding Mode Control Design for a Low-Lift Reentry Vehicle

AbstractIn this paper, a multioutput trajectory control of a reentry vehicle is presented. Adaptive fuzzy sliding mode control with an adjustable structure of the membership function is employed. The main goal of the adjustable structure is that the span of the membership function covers all the variations of the fuzzy inputs. The fuzzy inputs include the altitude, velocity, and flight path angle of the vehicle. The sliding surface is designed in two steps. At the first step, the error of the flight path angle is solely employed. Then, to improve the performance, the altitude and velocity of the reentry are added to sliding surface. The stability of the closed loop system is proven on the basis of the Lyapunov approach. To consider performance of the closed loop system, some simulations are done. The results show outperformance of the proposed method.

[1]  Ashish Tewari Atmospheric and space flight dynamics , 2006 .

[2]  Mohammad Bagher Menhaj,et al.  Adaptive fuzzy model based predictive control of nuclear steam generators , 2007 .

[3]  Mohammad Bagher Menhaj,et al.  A single fuzzy rule to smooth the sharpness of mixed data: Time and frequency domains analysis , 2008, Fuzzy Sets Syst..

[4]  Romeo Negrea,et al.  Optimal control in trajectory planning for a re-entry vehicle , 2008 .

[5]  J. Peter Reding,et al.  Lifting entry rescue vehicle configuration , 1990 .

[6]  Axel J. Roenneke,et al.  Trajectory control for a low-lift re-entry vehicle , 1993 .

[7]  Axel J. Roenneke,et al.  Nonlinear drag-tracking control applied to optimal low-lift reentry guidance , 1996 .

[8]  Jan Albert Mulder,et al.  Fuzzy logic based full-envelope autonomous flight control for an atmospheric re-entry spacecraft ☆ , 2003 .

[9]  Tao Zhang,et al.  Direct adaptive control of non-affine nonlinear systems using multilayer neural networks , 1998, Proceedings of the 1998 American Control Conference. ACC (IEEE Cat. No.98CH36207).

[10]  Jan Albert Mulder,et al.  Nonlinear dynamic modeling and simulation of an atmospheric re-entry spacecraft ? ? This paper was f , 2001 .

[11]  Ian Postlethwaite,et al.  Robustness analysis of a reusable launch vehicle flight control law , 2009 .

[12]  R. Wingrove SURVEY OF ATMOSPHERE RE-ENTRY GUIDANCE AND CONTROL METHODS , 1963 .

[13]  A. Rubaai Direct adaptive fuzzy control design achieving H/sup /spl infin// tracking for high performance servo drives , 1999 .

[14]  Ashish Tewari,et al.  Adaptive maneuvering entry guidance with ground-track control , 2007 .

[15]  Radhakant Padhi,et al.  Suboptimal reentry guidance of a reusable launch vehicle using pitch plane maneuver , 2010 .

[16]  A. Cavallo,et al.  Atmospheric re-entry control for low lift/drag vehicles , 1996 .

[17]  Seyed Mostafa Safavi,et al.  A novel FLC-based approach for ATM traffic control , 2001, Comput. Networks.