Not Applicable
Not Applicable
The present invention is related to the field of navigational systems and devices and, more particularly, to navigational systems and devices capable of detecting inclination and changes in inclination of an object in motion without having to compensate for the acceleration of the object.
Presently, on-board, three-dimensional travel navigation systems using, for example, the global positioning system (“GPS”), compensate for vehicle acceleration by using a speed pulse that is generated by a speed-pulse generator to accurately detect inclination of the vehicle.
Recent car makes and models can be digitally wired, e.g., using a CAN bus connection, to provide the speed pulse. Transducers have been used to produce speed pulses in older model vehicles. Another popular system incorporates a magnetized, steel, bias wire in one of the vehicle's tires. A receiver is adapted to count the number of rotations of the tire, generating an electronic speed pulse after a predetermined number of rotations.
It would be desirable to provide a system or a device that does not rely on speed pulses, which is to say that the system or device detects inclination independent of the acceleration of the object.
A system and device for detecting inclination that eliminates the need to compensate for the acceleration of the object is disclosed. The system includes a multi-axis, e.g., two-axis, acceleration sensing device that is fixedly attached to the object such that each sensing axis of the multi-axis acceleration sensing device lies in a common plane with the forward-aft axis of the object. The sensing axes are orthogonal to one another and are oriented 45 degrees from each side of the forward-aft axis.
Also disclosed is a method of determining an inclination associated with an object in motion, which includes sensing the acceleration of the object using a multi-axis acceleration sensing device that is fixedly attached to the object; and calculating the inclination of the object (a) using the equation:
in which g is the acceleration due to gravity, ax is a sensed acceleration along a first sensing x-axis and ay is a sensed acceleration along a second sensing y-axis.
Other aspects, features, and advantages of the present invention will be apparent from the Detailed Description that follows.
The invention will be better understood by reference to the following more detailed description and accompanying drawings where like reference numbers refer to like parts:
According to the present invention, a two-axis accelerometer 15 can be mounted on the accelerating object 10 so that each of the two sensing axes 11 and 13 lie in a common plane (the xy-plane 12) and so that the two sensing axes 11 and 13 are orthogonal to each other. Each of the sensing axes 11 and 13 of the two-axis accelerometer 15 are fixedly positioned to the accelerating object 10 to be 45 degrees from the forward-aft axis 14 of the accelerating object 10, wherein the forward-aft axis 14 of the accelerating object 10 also lies in the same xy-plane 12.
For example, the two-axis accelerometer 15, such as the accelerometers manufactured by MEMSIC, Inc. of Andover, Mass., is a monolithic structure that can be fixedly attached to a daughter printed circuit board (PCB), which, in turn, can be vertically mounted on a main PCB.
As shown in
Because each of the sensing axes 11 and 13 of the two-axis accelerometer 15 are fixedly positioned to the accelerating object 10 to be 45 degrees from the forward-aft axis 14 of the object 10, the relationship between sensed acceleration in the x-direction ax and the rate of acceleration ac of the object 10 and the relationship between sensed acceleration in the y-direction ay and the rate of acceleration ac of the object 10 are given by the following identities:
The relationship between sensed acceleration in the x-direction ax and the acceleration of gravity g and the relationship between sensed acceleration in the y-direction ay and the acceleration ac of gravity are given by the following identities:
Since β=90°−α, equation [4] also can be expressed as
Summing the accelerations in equations [1] through [4],
Σ(ax+ay)=g*cos α+ac*sin 45°+g*sin α−ac*cos 45° [6]
which can be reduced to:
Σ(ax+ay)=g*cos α+g*sin α [7].
Thus,
ax+ay=g(cos α+sin α) [8],
or
ax+ay=√
Solving for the first angle α between the line 16 and the axis 11 of the sensed acceleration in the x-direction ax:
In short, the first angle α between the line 16 and the axis 11 of the sensed acceleration in the x-direction ax is independent of vehicle acceleration ac and, hence, use of a speed pulse is unnecessary.
As
To ascertain whether the accelerating object 10 is traveling up or traveling down an incline, after solving for the first angle α using equation [10], instantaneous accelerations a1 and a2 can be determined using the following equations:
a1=g*cos α [11] and
a2=g*sin α [12].
If the difference of ax−a1 is approximately equal to the difference of ay−a2 then the accelerating object 10 is traveling up an incline. Alternatively, if the difference of ay−a1 is approximately equal to the difference of ax−a2 then the accelerating object 10 is traveling down an incline.
To improve the signal-to-noise ratio (SNR), the signal from the accelerometer can be passed through a low-pass filter, which reduces noise. Additionally or alternatively, SNR can be improved by mounting two accelerometers vertically so that they are oriented in opposite directions, which is to say that one accelerometer is mounted on the forward-aft axis of the accelerating object and the other accelerometer is mounted on the backward-aft axis of the accelerating object. Output from the two accelerometers would provide a signal having twice the magnitude, further diminishing the SNR.
Referring to
Although the invention has been described assuming a two-axis accelerometer in which the two axes are located in the xy-plane, this is not to say that the two axes could not also be oriented in the xz- or the yz-plane. With either of these latter arrangements, a common mode signal based on acceleration and deceleration due to inclination would replace, instead, by a common mode signal in a direction normal to the direction of travel. As a result, signal noise from the road surface can be reduced.
Although the invention has been described using a wheeled-vehicle as the accelerating object, the invention is not to be construed as being limited thereto. For example, the accelerating object could be a tracked-vehicle, sea- or ocean-going vessel, an aircraft, a spacecraft, a satellite, a digital camera, and the like.
It will be apparent to those skilled in the art that modifications to and variations of the disclosed methods and apparatus are possible without departing from the inventive concepts disclosed herein, and therefore the invention should not be viewed as limited except to the full scope and spirit of the appended claims.
Number | Name | Date | Kind |
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20060080033 | Komatsu | Apr 2006 | A1 |
20070173997 | Shiozawa et al. | Jul 2007 | A1 |
20070265085 | Miyamoto et al. | Nov 2007 | A1 |
Number | Date | Country | |
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20100004893 A1 | Jan 2010 | US |