The characteristic model-based golden-section adaptive control (CM-GSAC) law has been developed for over 20 years in China with a broad range of applications in various fields. However, quite a few theoretical problems remain open despite its satisfying performance in practice. This paper revisits the stability of the CM-GSAC from its very beginning and explores the underlying implications of the so-called golden-section parameter l 2 0:618. The closed-loop system, which consists of the CM and the GSAC, is a discrete time-varying system, and its stability is discussed from three perspectives. First, attentions have been paid to select the optimal controller coefficients such that the closed-loop system exhibits the best transient performance in the worst case. Second, efforts are made to improve the robustness in the presence of parameter estimation errors, which provide another choice when designing the adaptive controller. Finally, by measuring the slowly time-varying nature in an explicit inequality form, a bridge is built between the instantaneous stability and the time-varying stability. In order to relax the constraints on the parameter bounds of the CM, the GSAC is further extended to multiple CMs, which shows more satisfying tracking performance than that of the traditional multiple model adaptive control method.
878H. HUANG
INTRODUCTIONAs being mentioned in [1], 'It is always better to use an accurate model than not to do so: if there is time delay present and it is neglected, or if there are high frequency dynamics present and they are neglected, an algorithm is more likely to fall over'. However, in practical applications such as the attitude control of hypersonic vehicles that are characterized by strongly coupled multiple states, nonlinearity, high order, and, most importantly, the lack of ground test facilities, it would be rather complicated to develop controllers based on the accurate dynamical model that is highly nonlinear with various uncertainties. Meanwhile, the dynamic performance during controller design is usually unknown when dealing with the nonlinear dynamics directly. A common way is to use the linearization technique at several preselected operation points, for example, the trim conditions of hypersonic vehicles, so as to develop linear controllers. This would be time consuming because of a tremendous amount of points if the vehicle maneuvers frequently and flies in a rapidly changing environment. Meanwhile, controller design based on the linearized model generally lacks adaptability and flexibility. The characteristic model (CM)-based adaptive control thus appears so as to build a bridge between the model complexity and the adaptability.The CM was proposed by Hongxin Wu in the 1990s and has further been developed for more than 20 years [2,3]. The essence of the CM is to use a low-order discrete time-varying system to approach a high-order nonlinear/linear system based on the main features of the plant and the control demands. Rather than dropping information as in the reduced-order m...