Trajectory planning of differentially flat systems with dynamics and inequalities

被引:104
作者
Faiz, N [1 ]
Agrawal, SK
Murray, RM
机构
[1] Univ Delaware, Dept Mech Engn, Mech Syst Lab, Newark, DE 19716 USA
[2] CALTECH, Dept Mech Engn, Div Engn & Appl Sci, Pasadena, CA 91125 USA
关键词
D O I
10.2514/2.4732
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Trajectory planning of dynamic systems, in near real time, is important for aerospace systems, especially uncrewed air vehicles and launched munitions. Trajectory plans that do not consider the governing dynamic equations, applicable path, and actuator constraints may be unrealizable during execution. A trajectory planning scheme is proposed for a class of dynamic systems, referred to as differentially hat systems. The planner is motivated from online computations and is aimed to satisfy the state equations, path and actuator constraints, and given initial and terminal constraints. The essence of the approach is demonstrated by two examples: 1) a hardware implementation on a spring-mass-damper system to demonstrate real-time capabilities during pursuit and 2) trajectory planning of a planar vertical takeoff and landing aircraft to illustrate the application to nonlinear problems.
引用
收藏
页码:219 / 227
页数:9
相关论文
共 19 条
  • [1] AGARWAL SK, 1998, J OPTIMIZATION THEOR, V97, P11
  • [2] AGARWAL SK, 1996, J DYNAMIC SYSTEMS ME, V118, P786
  • [3] [Anonymous], 1960, COMBINATORIAL ANAL
  • [4] BEULER B, 1999, DMV SEMINARS SERIES
  • [5] Bryson AE., 1975, Applied optimal control: optimization, estimation and control
  • [6] Cheney E.W., 1959, Numerical Mathematics, V1, P253, DOI DOI 10.1007/BF01386389
  • [7] *ECP ED PROD INC, 1996, MAN MOD 210 210A REC
  • [8] FLETCHER CAJ, 1984, COMUTATIONAL GALERKI
  • [9] FLATNESS AND DEFECT OF NONLINEAR-SYSTEMS - INTRODUCTORY THEORY AND EXAMPLES
    FLIESS, M
    LEVINE, J
    MARTIN, P
    ROUCHON, P
    [J]. INTERNATIONAL JOURNAL OF CONTROL, 1995, 61 (06) : 1327 - 1361
  • [10] GLOVER F, 1975, MATH PROGRAM, V8, P161