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1.?Introduction
With
the rapid development of the micro-optical-electro-mechanical systems
(MOEMS) technology, the micromation of the payloads in micro-satellites
has become a general trend [1].
For optical scanning and target detection, the laser scanning technique
is an active way to detect objects and measure both range and
orientation [2].
The two-dimensional scanning micro-mirror has great advantages over the
conventional scanning mechanisms, such as low power consumption, small
volume and high frequency. It has a broad range of space applications
for target detection in micro-satellites. At present, most of scanning
micro-mirrors have been driven by electrostatic, electromagnetic or
piezoelectric force. They have a spring structure and are operated on a
resonant mode for high-speed scan operation with large deflection [3–7].
For target detection and location, the scanning micro-mirror requires
the measurement of deflection angles with high sensitivities, which most
of the current researches have not involved. A LIDAR (LIght Detection
And Ranging) system with a magnetic mirror and a micro shutter array is
adopted for planetary explorer [2],
but the mechanism is complicated and the scanning field is narrow. A
laser range finder coupled with two silicon micro-mirrors are used in
the compact robotics perception system [8],
but adopting a PSD sensor for position detection decreases the
integration of the system. A MEMS electromagnetic optical scanner for a
laser scanning microscope integrated sensing coil for deflection angle
measurement [9], but the scanner is one-dimensional and the induced electromotive force is low with limited sensitivity.
With
the aim of improving these deficiencies, a two-dimensional scanning
micro-mirror with piezoresistor sensors for measurement of deflection
angles is developed in this paper. It has a simple structure and a small
volume, with a large scanning field and high sensitivities. Based on
the scanning micro-mirror and the phase-shift ranging technology, a
MOEMS target detector has also been developed. In the last section, the
performance of the prototype and experimental results will be described
in detail.
2.?Two-Dimensional Scanning Micro-Mirror
2.1. Structure
A two-dimensional scanning micro-mirror with a piezoelectric actuator and piezoresistors was designed as shown in Figure 1.
The micro-mirror structure consists of a reflector, an inertia
generator, a flexible beam and an excited part, which is 8 mm × 8 mm ×
0.2 mm in size. The reflector and inertia generator are formed together,
and linked with the excited part by the flexible beam. The excited part
is connected to the piezoelectric actuator. The piezoresistors are
integrated on the surface of the flexible beam for deflection angles
measurement [10].
Structure of the two-dimensional scanning micro-mirror.
The
piezoelectric actuator deforms along the z-axis by pulsant driving
voltage and the excited part vibrates in the z-axis. As the center of
gravity of the reflector and inertia generator is away from each
rotational axis (x and y), the micro-mirror has two resonance vibration
modes: twisting around the y-axis and bending around the x-axis, as
shown in Figure 2.
The two-dimensional micro-mirror is thus equivalent to a two
dimensional vibration system with two different resonant frequencies.
Actuating the micro-mirror at each resonant frequency can make the
mirror vibrate with large deflection angles θT and θB around
the y-axis and x-axis, respectively. When a resultant voltage including
two different resonant frequencies is imposed to the piezoelectric
actuator, both vibration modes are excited and the micro-mirror is
capable of scanning a light beam two-dimensionally with large scanning
angles with a single driving source.
Two resonance vibration modes. (a) twisting around the y-axis, (b) bending around the x-axis.
2.2. Piezoresistors
Deflection
angle sensing is based on the piezoresistive effect, which has the
advantages of favorable dynamic characteristics and high sensitivities.
The surface stresses generated on the flexible beam when the
micro-mirror is twisting or bending and piezoresistors are laid on the
flexible beam for the deflection angles measurement of two directions.
The change of the resistance in piezoresistor is related to the stresses
and the piezoresistive coefficients in longitudinal, transverse and
tangential directions. The piezoresistive effect in plane can be
described as follows [11]:
ΔRR=πlσl+πtσt+πτστ,
(1)
where σl is the longitudinal stress, σt is the transverse stress and στ is the tangential stress. πl is the longitudinal coefficient, πt is the transverse coefficient and πτ is the tangential coefficient.