Design and Realization of Modular MEMS-Based Attitude Measurement and Control System Based Wireless Sensor Networks

2012 ◽  
Vol 503 ◽  
pp. 393-396
Author(s):  
Shao Peng Liu ◽  
Zhao Ying Zhou ◽  
Xing Yang ◽  
Qiu Sheng Liu ◽  
Qiong Wang ◽  
...  
Keyword(s):  
Control System ◽  
Flight Control ◽  
Control Unit ◽  
Measurement Unit ◽  
Attitude Measurement ◽  
Measurement And Control System ◽  
Central Processing ◽  
High Efficient ◽  
And Control ◽  
Measurement And Control

The Modular Platform System in this Paper Consists of a Series of Modularized MEMS Subsystems, Including Central Control Unit, MEMS Attitude Measurement Unit, Environment Unit, Flight Measurement and Control Unit, Time Control Unit, Impact Vibration Measurement Unit and other Auxiliary Modular Units. the Key of the System Is the MEMS Attitude Measurement Unit, which Can Resolve the Real Time Attitude Information of the Carrier. the System Platform Chooses Different Sensors and Units According to Various Circumstances and Implements Data Collection, Fusion and Solution through the Central Processing Module. by Means of Carrying Distinct Units, System Platform Can Constitute many Measurement Control Systems, such as Micro Wireless Attitude Determination System, MAV Flight Data Recorder, MAV Flight Control System and PHM (prognostic and Health Management). with Application of MEMS, the System in this Paper Is High-Efficient, Low-Weighted, Simple-Structured, High-Reliable and even Can Respond in a Short Time. in View of these Merits, the System Can Be Applied in many Kinds of Attitude Measurement and Control System.

scholarly journals The Attitude Measurement and Control System of EURECA

1987 ◽  
Vol 20 (5) ◽  
pp. 89-101
Author(s):  
P. Bourg ◽  
B. Cyna ◽  
Y. Martinet ◽  
E. Brüderle ◽  
T. Bückle ◽  
...  
Keyword(s):  
Control System ◽  
Attitude Measurement ◽  
Measurement And Control System ◽  
And Control ◽  
Measurement And Control

Design of MMFCS for MAV Based on MEMS Sensor

2011 ◽  
Vol 483 ◽  
pp. 542-547
Author(s):  
Wei Xiong ◽  
Zhao Ying Zhou ◽  
Xiao Yan Liu
Keyword(s):  
Control System ◽  
Flight Control ◽  
Minimum Size ◽  
Fusion Algorithm ◽  
Micro Aerial Vehicle ◽  
Measurement And Control System ◽  
Mems Sensor ◽  
Aerial Vehicle ◽  
And Control ◽  
Measurement And Control

Micro Measurement and Flight Control System (MMFCS) is important for an autonomous Micro Aerial Vehicle (MAV) to accomplish a flight task. Being in small size, low speed and limited payload capacity, most conventional measurement and control system is no longer practical in Micro Aerial Vehicle (MAV). In this paper presents a study on micro-MMFCS system based on criteria of minimum size and low computational complexity to complete the autonomous fly. Via using MEMS sensors, the developed micro MMFCS is with a size of 65×40×12mm3 and a weight of 22g. A novel linear fusion algorithm with a linear (and simple) Kalman model is presented to get the roll and pitch angle, then, the controller is designed in the lateral and longitudinal control loop for the trajectory tracking. Examples of waypoint-based autonomous fly mission, using the micro-MMFCS system of a MAV with a wingspan of 380 mm, is presented, with the results demonstrate the effectiveness of the proposed system.

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