Abstract
In this paper, a disturbance observer based optimal attitude control scheme using \(\theta -D\) method is presented for the near space vehicle (NSV). Firstly, \(\theta -D\) method is used to design the optimal controller for the nominal system without considering the disturbance. Secondly, nonlinear disturbance observer (NDO) technique is applied to estimate the disturbance and the estimation result can be used as the disturbance compensation term. Then, the composite controller consisting of optimal controller and disturbance compensation term is proposed. The closed-loop system signals are proved to be uniformly ultimately bounded (UUB) using Lyapunov method. Finally, simulation results show the effectiveness of proposed control scheme.
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References
Liu, Z., Tan, X.M.: Adaptive trajectory tracking control system design for hyoersonic vehicles with parametric uncertainty. Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 229(1), 182–187 (2015)
Li, Y., Wu, Q.X., Jiang, C.S.: Robust predictive control for hypersonic vehicles using recurrent functional link artificial neural networks. Int. J. Innovation Comput. Inf. Control. 6(12), 5351–5365 (2010)
Xu, B., Zhang, Q., Pan, Y.P.: Neural network based dynamic surface control of hypersonic flight dynamics using small-gain theorem. Neurocomputing 173, 690–699 (2016)
Gao, Z.F., Jinag, B., Qi, R.Y.: Robust reliable control for a near space vehicle with parametric uncertainties and actuator faults. Int. J. Syst. Sci. 42, 2113–2124 (2011)
Ge, S.S., Wang, C.: Adaptive neural control of uncertain MIMO nonlinear systems. IEEE Trans. Neural Netw. 15, 674–692 (2004)
Xin, M., Balakrishnan, S.N., Stansbery, D.T.: A new method for suboptimal control of a class of nonlinear systems. Optim. Control Appl. Method 26, 55–83 (2005)
Xin, M., Balakrishnan, S.N.: Nonlinear missile autopilot with theta-D technique. J. Guidance Control Dyn. 27, 406–417 (2004)
Xin, M.: Trajectory control of miniature helicopters using a unified nonlinear optimal control technique. In: Aiaa Guidance, Navigation, and Control Conference, pp. 2417–2424 (2013)
Liu, R.J., Li, S.H., Chen, X.S.: Powered-decent trajectory optimization scheme for Mars landing. Ad. Space Res. 52(11), 1888–1901 (2013)
Chen, W.H., Ballance, D.J., Cawthrop, P.J.: A nonlinear disturbance observer for robotic manipulators. IEEE Trans. Industr. Electron. 47(4), 932–938 (2000)
Chen, M., Jiang, B.: Robust attitude control of near space vehicles with time-varying disturbances. Int. J. Control Autom. Syst. 11(1), 182–187 (2013)
Chen, M., Yu, J.: Disturbance observer-based adaptive sliding mode control for near space vehicles. Nonlinear Dyn. 82(4), 1671–1682 (2015)
Du, Y.L., Wu, Q.X., Wang, Y.H.: Adaptive robust predictive control for hypersonic vehicles using recurrent functionl link artificial neural networks. Int. J. Innovation Comp. Inf. Control 6(12), 5351–5365 (2010)
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Appendix
Appendix
Proof:
Choose a Lyapunov candidate function
Taking the time derivative of (13), we have
Since \(u=-R^{-1}g^T(x)\sum \limits _{i = 0}^\infty {{{\hat{T}}_i}}x-g^{-1}(x)\hat{d}\), then we have
where \(\bar{\lambda }=\lambda _{min}[Q+\sum \limits _{i = 0}^\infty {D_i\theta ^i}]\).
Using the relationship \(\frac{\partial \hat{T}_i}{\partial x}=\epsilon _i\frac{\partial \bar{T}_i}{\partial x}\), we have [6]
Note that as long as x lies in a compact set with A(x) is bounded; g(x) is bounded as shown in Assumption 1; \(\sum \limits _{i = 0}^\infty {{\hat{T}_i(x)}}\) is converge and positive in Lemma 1, one can always choose a set of \(\epsilon _i\) such that
then we have
If \(\Vert x\Vert >\sqrt{\frac{B_d}{M}}\) or \(\Vert \tilde{d}\Vert >\sqrt{\frac{B_d}{N}}\), we have \(\dot{L}(t)< 0\), then the disturbance estimation error \(\tilde{d}\) and system states x are proved to be UUB.
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Xia, R., Wu, Q., Yan, X. (2017). Disturbance Observer Based Optimal Attitude Control of NSV Using \(\theta -D\) Method. In: Liu, D., Xie, S., Li, Y., Zhao, D., El-Alfy, ES. (eds) Neural Information Processing. ICONIP 2017. Lecture Notes in Computer Science(), vol 10639. Springer, Cham. https://doi.org/10.1007/978-3-319-70136-3_24
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DOI: https://doi.org/10.1007/978-3-319-70136-3_24
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