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**Active fault tolerant control design for reusable launch vehicle using adaptive sliding mode technique.**
*(English)*
Zbl 1253.93018

Summary: In this paper, the problem of active fault tolerant control for a Reusable Launch Vehicle (RLV) with actuator fault using both adaptive and sliding mode techniques is investigated. Firstly, the kinematic equations and dynamic equations of RLV are given, which represent the characteristics of RLV in reentry flight phase. For the dynamic model of RLV in faulty case, a fault detection scheme is proposed by designing a nonlinear fault detection observer. Then, an active fault tolerant tracking strategy for RLV attitude control systems is presented by making use of both adaptive control and sliding mode control techniques, which can guarantee the asymptotic output tracking of the closed-loop attitude control systems in spite of actuator fault. Finally, simulation results are given to demonstrate the effectiveness of the developed fault tolerant control scheme.

### MSC:

93B12 | Variable structure systems |

93C40 | Adaptive control/observation systems |

93B51 | Design techniques (robust design, computer-aided design, etc.) |

### Keywords:

reusable launch vehicle (RLV); adaptive mode techniques; sliding mode techniques; active fault tolerant tracking; closed-loop attitude control
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\textit{Z. Gao} et al., J. Franklin Inst. 349, No. 4, 1543--1560 (2012; Zbl 1253.93018)

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### References:

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