The present invention relates to MEMS (micro-electromechanical systems) technology, in particular to MEMS employing optical micro-sensors for measuring rate rotation.
Micro-electro-mechanical systems (MEMS) provide an electrical output in response to movement. MEMS are being incorporated in an increasing number of sensor and actuator devices especially in applications making use of orientation, alignment and stabilization such as medical devices, photographical equipment, transportation navigation and inertial sensors, and defense applications. MEMS are produced using several known microprocessing techniques, including: photolithography, wet etching, dry etching, physical vapor deposition, chemical-vapor deposition, oxidation, etc.
Micro-opto-electromechanical systems (MOEMS) constitute a special class of MEMS which involves sensing or manipulating optical signals using integrated mechanical and electrical systems.
Micro-electromechanical optical inertial sensing devices that measure rotation rate, typically make use of the Coriolis effect to detect rotation rate. U.S. Pat. No. 6,350,983, the contents of which are incorporated herewith by reference, discloses such a micro-machined optical inertial sensing device (sensor) in which a MEMS proof mass is suspended on cantilevers. U.S. Pat. 7,071,594 discloses a MEMS scanning device which is another application of optical MEMS.
The present invention is implemented in the framework of a specific type of electro opto-mechanical rotation rate sensing system, which is a rotation rate measuring system, the basic structure of which is described in U.S. Pat. No. 7,091,715, and the details of which are incorporated herein by reference. In brief, a proof mass hanging on beams is installed on top of a VLSI circuit such that the movement of the proof mass is not impaired. A mechanism is provided for driving the proof mass as known in the art. Any change in the mechanical forces acting on the sensor would create a response on the otherwise predicted motion of the proof mass. The movement of the proof mass is monitored by an array of light sensitive photo-detectors attached to the VLSI component, as the shade effected by the proof mass, masking the light of an illumination source, changes in coverage in one or more dimensions, in a time dependent fashion.
The motivation of the invention is to better exploit the dynamic range of the hardware infrastructure provided by the optical electro-mechanical rotation sensor on board the MOEMS in conditions of varying input signal level. Accordingly, such a sensor together with its circuitry can be adapted before the mission or modified autonomously during a mission to a specific range of mechanical stimuli, to optimally exploit the available dynamic range and thereby enhance the performance of the microdevice. The specific MOEMS in which the present invention is implemented will be referred to as Micro-opto-electromechanical rotation rate sensor (MOERRS).
The invention may be understood upon reading of the following detailed description of non-limiting exemplary embodiments thereof, with reference to the following drawings, in which:
The output signal (in volts) of a Micro-opto-electromechanical rotation rate sensor (MOERRS) device in which the invention is implemented, is referred to hereinafter as Vsense. This output signal is related to the mechanical rotation observed by the sensor, and can be described as relating generally to several variables, in equation 1:
V
sense
=f(Gelectronic, Goptical, Gmechanical, Yexc, Ωrate)
Where: Gelectronic is the electronic gain
Goptical is the optical gain,
Gmechanical is the mechanical gain
Yexc is the mechanical excitation
Ωrate is the value of the input signal, in rotational units of the sensor.
In accordance with the present invention, some components of a MOEMS are made such that a. pre-mission modifications can be made to adapt the MOEMS to a specific range of mechanical rotation values expected to occur within the mission, and b. within-mission modifications can be made to adapt the MOEMS to changing mechanical rotation value ranges within the mission. As inferred by equation 1 above, the output signal value (in volts) can be adapted to within limits of the dynamic range by implementing several discrete control loops in the MOEMS, to optimally exploit the dynamic range of the MOERRS.
1. The Mechanical Adaptation
In general, the output mechanical signal of a MOERRS, is a product of the cyclical excitation signal. Thus, in order to increase the output signal, an increase in the excitation rate (i.e. the excitation signal) is effected, thereby providing higher signal values in the output of the sensor. The lower the input rotation signal is, the higher the excitation rate to be applied is in order to bring the output signal to a specific optimal range of values. In order to adapt the MOERRS pre-mission, a specific excitation rate value is to be selected in order to accommodate the expected output values of the sensor to the available dynamic range. Within-mission adaptation, requires the implementation of a control loop that controls the excitation rate by adaptively changing the excitation range. Although somewhat obvious to a person skilled in the art of control mechanisms, it is explained with reference to
2. The Electronic Control (Loop)
In combination with the above mechanical control mechanism or without such linkage, modifications in the electronic circuitry level can be used to bring the output signal of the sensor to such a range of values as to exploit the given dynamic range of the MOEMS device. The MOERRS which is implemented in a VLSI chip containing also additional elements, and peripheral circuitry disposed besides the MOERRS which supports the VLSI, for example accepting the amplified varying signal and amplifying it and conditioning it further. In accordance with the present invention, the output signal of the sensor is modified either on the VLSI chip or within the peripheral circuitry to accommodate the signal to appropriate ranges, to exploit the given dynamic range under a range of mechanical stimuli.
Peripheral Circuits Adaptation
The optical sensor on the VLSI chip, includes typically an array of photo detectors (typically photodiodes). Each such photo detector or some of them is connected to a switch and can be switched on or off. As can be seen in
In another embodiment of the invention, described in a scheme in
On-VLSI Amplification Adaptation
On the VLSI, respective amplifiers that receive current from the various photo sensitive elements of the photo sensitive detectors array are monitored individually. As can be seen in
3. The Optical Control (Loop)
The light impinging on the optical sensor array, causes the ejection of electrons from the photo-sensitive portions of the detectors, creating a current that relates to the mechanical stimulus, and therefore can be used to measure the mechanical stimulus effecting the MOEMS. To enable the MOERRS and the MOEMS in general to exploit its full dynamic range for the measurement of the mechanical stimulus, the current/impinging light ratio can be changed in several ways. As can be seen in
Such slits are possibly implemented by adding to the MOEMS architecture a perforated plate as can be seen in the scheme shown in
Pre-mission adjustment of the MOEMS can take into account the expected magnitude of the mechanical stimuli expected in the mission. For higher the expected stimuli, more shutters can be closed allowing for less light to reach the photo-sensitive arrays. Vice versa, for missions in which mechanical stimuli of lesser magnitude are expected, more exposure is to be effected. Within-mission control loop of exposure to the photo sensitive array can be effected by measuring the signal of the MOERRS and responding by shutting available perforations if signal is too high, and vice versa. A variety of perforation closure control embodiment can be effected by superimposing LED screens over respective perforations, so that shutting can be implemented by turning on LED photodiode disposed over a perforation, such that the pigmentation formed reduces the amount of light penetration through the respective perforation.
Number | Date | Country | Kind |
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202712 | Dec 2009 | IL | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IB2010/055789 | 12/14/2010 | WO | 00 | 6/6/2012 |