Observer-based digital tracker for the manoeuvring target described by the continuous-time non-linear dynamic system

被引:1
作者
Tsai, J. S. H. [1 ]
Wang, C. T. [1 ]
Guo, S. M. [2 ]
Shieh, L. S. [3 ]
Liu, C. R. [3 ]
机构
[1] Natl Cheng Kung Univ, Dept Elect Engn, Tainan 701, Taiwan
[2] Natl Cheng Kung Univ, Dept Comp Sci & Informat Engn, Tainan 70101, Taiwan
[3] Univ Houston, Dept Elect & Comp Engn, Houston, TX USA
关键词
digital tracker; guidance law; optimal linearization; digital redesign; interception time;
D O I
10.1243/09544100JAERO238
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The current paper develops an effective and robust digital guidance law to intercept the highly manoeuvring target described by the continuous-time non-linear dynamic system. First, an optimal linearization model for the non-linear system is constructed at the operating point of interest on the trajectory. Then, high-gain optimal linear quadratic analogue tracker and observer are designed by utilizing the optimal linearization model and the optimal control theory, so that the effect of the unpredictable acceleration of the target can be substantially attenuated and even can be disregarded. For reducing the control effort without raising the prescribed interception time, and for practical implementation of the designed tracker, the prediction-based digital redesign method is utilized to obtain relatively low-gain digital tracker and observer from the well-designed high-gain optimal analogue tracker and observer. With the aid of the global positioning system, the proposed observer-based digital tracker is able to successfully intercept a highly manoeuvring target without the constraint on initial trajectory, and can effectively deal with various barriers during the interception. Illustrative examples are given to demonstrate the effectiveness and robustness of the proposed digital guidance law.
引用
收藏
页码:213 / 228
页数:16
相关论文
共 24 条
[1]  
ATHANS M, 1966, OPTIMAL CONTROL, P793
[2]   H-INFINITY CONTROL FOR NONLINEAR-SYSTEMS WITH OUTPUT-FEEDBACK [J].
BALL, JA ;
HELTON, JW ;
WALKER, ML .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1993, 38 (04) :546-559
[3]  
Bryson A., 1969, APPL OPTIMAL CONTROL, P148
[4]   Nonlinear fuzzy H∞ guidance law with saturation of actuators against maneuvering targets [J].
Chen, BS ;
Chen, YY ;
Lin, CL .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2002, 10 (06) :769-779
[5]   Parametric robustness evaluation of a H-infinity missile autopilot [J].
Ferreres, G ;
MSaad, M .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (03) :621-627
[6]   Effective chaotic orbit tracker: A prediction-based digital redesign approach [J].
Guo, SM ;
Shieh, LS ;
Chen, GR ;
Lin, CF .
IEEE TRANSACTIONS ON CIRCUITS AND SYSTEMS I-FUNDAMENTAL THEORY AND APPLICATIONS, 2000, 47 (11) :1557-1570
[7]   NONLINEAR H-INFINITY CONTROL AND ITS APPLICATION TO RIGID SPACECRAFT [J].
KANG, W .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1995, 40 (07) :1281-1285
[8]  
LEWIS FL, 1995, OPTIMAL CONTROL, P215
[9]  
LIN CF, 1991, MODERN NAVIGATION GU, V2, P252
[10]   A NEW LOOK AT CLASSICAL VS MODERN HOMING MISSILE GUIDANCE [J].
NESLINE, FW ;
ZARCHAN, P .
JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (01) :78-85