Control of wing for micro-airplane with smart material and laser

被引：0

作者：

Kajiwara, I ^{[1
]}

Ishikawa, H ^{[1
]}

Furuya, S ^{[1
]}

Yabe, T ^{[1
]}

Nishidome, C ^{[1
]}

机构：

[1] Tokyo Inst Technol, Dept Mech & Aerosp Engn, Meguro Ku, Tokyo 1528552, Japan

来源：

BEAMED ENERGY PROPULSION | 2003年 / 664卷

关键词：

D O I：

暂无

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

A laser tracking system and a smart wing are proposed and developed to control the flight of a laser-driven micro-airplane. The laser tracking system is composed of a light source, detector and optical system with a galvano-mirror control mechanism, and used for controlling the smart wing constituted by a wing, phototransistor, battery and smart material. The light source is installed on the ground and so this system is effective for miniaturization and lightening of the micro-airplane. Experiments are carried out to evaluate the performance of the laser tracking system and the smart wing.

引用

页码：545 / 556

页数：12

共 13 条

[1]

ISHIKAWA H, 2002, SICE ANN C 2002

[2]

JENN DC, 1997, P 1 INT C EM TECHN M, P74

[3] Integrated design of aerodynamics and control system for Micro Air Vehicles [J].

Kajiwara, I ;

Haftka, RT .

JSME INTERNATIONAL JOURNAL SERIES C-MECHANICAL SYSTEMS MACHINE ELEMENTS AND MANUFACTURING, 2000, 43 (03) :684-690

[4]

KAJIWARA I, 2001, P AIAA 42 SDM C

[5]

KAJIWARA I, 1999, P AIAA 40 SDM C, P1612

[6]

KANTROWI.A, 1972, ASTRONAUT AERONAUT, V10, P74

[7]

Morrel S, 1997, P 1 INT C EM TECHN M, P117

[8]

MYRABO LN, 1998, 36 AER SCI M EXH

[9] LISP - LASER IMPULSE SPACE PROPULSION [J].

PHIPPS, CR ;

MICHAELIS, MM .

LASER AND PARTICLE BEAMS, 1994, 12 (01) :23-54

[10] IMPULSE COUPLING TO TARGETS IN VACUUM BY KRF, HF, AND CO2 SINGLE-PULSE LASERS [J].

PHIPPS, CR ;

TURNER, TP ;

HARRISON, RF ;

YORK, GW ;

OSBORNE, WZ ;

ANDERSON, GK ;

CORLIS, XF ;

HAYNES, LC ;

STEELE, HS ;

SPICOCHI, KC ;

KING, TR .

JOURNAL OF APPLIED PHYSICS, 1988, 64 (03) :1083-1096

← 1 2 →