Human-inspired control logic for automated maneuvering of miniature helicopter

被引:31
作者
Gavrilets, V [1 ]
Mettler, B [1 ]
Feron, E [1 ]
机构
[1] MIT, Informat & Decis Syst Lab, Dept Aeronaut & Astronaut, Cambridge, MA 02139 USA
关键词
D O I
10.2514/1.8980
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The maneuvering control logic that was developed to implement aerobatic maneuvers fully automatically on a miniature helicopter is described. The key component of this system is a state-machine maneuver execution logic that was inspired by an analysis of human pilot strategies. Conventional multivariable trim trajectory controllers were used before and on the exit from the maneuvers; bumpless transfer between these control modes was achieved through re-initialization of controller integrator states. Flight tests with this control logic demonstrated smooth maneuver entry, automatic recovery to a steady-state trim trajectory, and an ability to sequence maneuvers in a fully autonomous airshow-like sequence. This approach was flight tested with split-S, hammerhead, and 360-deg axial roll maneuvers, as well as a split-S-hammerhead maneuver sequence. The maneuvering control logic can be used to automate a variety of other maneuvers.
引用
收藏
页码:752 / 759
页数:8
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