The Research of Embedded Techniques in Control Systems of Service Robots

A control system for service robots based on a 32-bit ARM processor with kernel S3C2410 is proposed. The entire structure of the control system of embedded service robots is designed in the paper. And designs of each circuit and software of the system are demonstrated respectively in detail. The control system proposed has advantages of modularized structure, small size, low power dissipation, hard real-time and high reliability, etc.

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Designing a Low-phase-noise, Low-power-dissipation CMOS-Ring VCO according to a New Figure of Merit

IEEJ Transactions on Electronics Information and Systems ◽

10.1541/ieejeiss.131.1397 ◽

2011 ◽

Vol 131 (8) ◽

pp. 1397-1402

Author(s):

Akio Momma ◽

Jun Ogura ◽

Eiji Nishimori

Keyword(s):

Low Power ◽

Phase Noise ◽

Power Dissipation ◽

Figure Of Merit ◽

Low Power Dissipation ◽

Low Phase Noise

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Low Power dissipation of Ring Counter using Dual sleep Transistor approach

i-manager’s Journal on Electronics Engineering ◽

10.26634/jele.4.3.2674 ◽

2014 ◽

Vol 4 (3) ◽

pp. 9-13

Author(s):

M. Balaji ◽

◽

B. Keerthana ◽

K. Varun ◽

◽

...

Keyword(s):

Low Power ◽

Power Dissipation ◽

Ring Counter ◽

Low Power Dissipation

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An AlGaAs/InGaAs pseudomorphic HEMT modulator driver IC with low power dissipation for 10 Gb/s optical transmission systems

1996 IEEE MTT-S International Microwave Symposium Digest ◽

10.1109/mwsym.1996.512205 ◽

2002 ◽

Cited By ~ 3

Author(s):

M. Miyashita ◽

M. Shimada ◽

N. Yoshida ◽

Y. Kojima ◽

T. Kitano ◽

...

Keyword(s):

Low Power ◽

Power Dissipation ◽

Optical Transmission ◽

Transmission Systems ◽

Optical Transmission Systems ◽

Low Power Dissipation ◽

Modulator Driver

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Second Paper: Failure-Survival Automatic Flight Control Systems for Aircraft with Particular Reference to a High Reliability Electrohydraulic Actuator

Proceedings of the Institution of Mechanical Engineers ◽

10.1243/pime_proc_1965_180_022_02 ◽

1965 ◽

Vol 180 (1) ◽

pp. 246-259

Author(s):

R. Ruggles

Keyword(s):

Control System ◽

Control Systems ◽

Flight Control ◽

High Reliability ◽

Supply System ◽

Design Criteria ◽

Flight Control System ◽

Advantages And Disadvantages ◽

System Configurations ◽

Very High

The author discusses some of the problems of failure-survival automatic flight control systems and suggests some basic ground rules as design criteria. The advantages and disadvantages of some of the main types of system are discussed: duplex, triplex, triple component, duplicate-monitored and quadruplex systems being covered. In particular, a quadruplex actuator is described which has been designed and developed mainly for automatic flight control system applications where a very high degrees of failure-survival capability is required. A detailed failure analysis of the various systems is carried out and the importance of the electrical and hydraulic supply system configurations and failure rates is brought out.

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