Autonomous formation flight

被引：313

作者：

Giulietti, Fabrizio ^{[1
]}

Pollini, Lorenzo ^{[1
]}

Innocenti, Mario ^{[1
]}

机构：

[1] Dept. of Elec. Syst. and Automation, University of Pisa, Via Diotisalvi 2, 56126 Pisa, Italy

来源：

IEEE Control Systems Magazine | 2000年 / 20卷 / 06期

关键词：

Aircraft - Control nonlinearities - Control system synthesis - Equations of motion - Global positioning system - Linearization - Mathematical models - Optimization - Position control - State space methods - System stability - Unmanned vehicles;

D O I：

10.1109/37.887447

中图分类号：

学科分类号：

摘要：

An approach to close-formation flight of autonomous aircraft was developed. A standard LQ-based structure was synthesized for each vehicle and for formation position error control using linearized equations of motion and a lifting line model of the aircraft wake. The resultant approach provides optimal path information sequencing in the nominal case, as well as the redundancy needed to accommodate failures in data transmission and reception.

引用

页码：34 / 44