Intended to communicate what is required to system developers and serve as the basis of a contract for the system development
1.0.0.0 Writing requirements definitions
An RSDIMU consists of a skewed array of redundant inertial sensors and examplifies
the current trend for designing hardware fault tolerant inerial measurement units
(IMU's) for high reliability applications. The portion of the RSDIMU you will handle
containes eight linear accelerometers mounted on the four triangular faces of a
semioctahedron.
Your procedure will have two functions, both of which are a consequence of the
redundancy in the sensor complement of the RSDIMU. The first function is to perform
a consistency check to detect and isolate failed sensors. The second is to use the sensors
found to be good by the first check to provide estimates of the vehicle's linear
acceleration expresses as components along the north, east, and down axes of a
navigational frame of reference.
. . . an RSDIMU as described here would operate as follows. With the vehicle
sttionary, as series of sensor readings would be taken over time, and this would comprise
the calibration data set for that particular flight. During flight, the sensors would be
read periodically at regular time intervals to provide input for the navigation software.
3. Physical structure:
The RSDIMU is composed of an instrument and a display. The display is
discussed in Section 6.3. This section is devoted to the structure of the instrument
package.
3.1 The instrument package is a semi-octahedron (a square-based pyramid) (Figure 1).
3.1.1 It has four non-base faces, named A, B, C, or D.
3.1.2 Each face contains two sensors, named the x and y sensors.
3.1.2.1 Associated with each sensor is a set of misalignment angles. These are specified further in Section 2.3.2.
Rationale: There is an ideal position for each sensor, but the physical mounting may differ slightly.
3.1.2.2 The misalignment angles are assumed to be small enough (less than 5 degrees) for the sine of the angle to be approximately equal to the value of the angle expressed in radians.
3.1.3 The temperature of the face, temp, determines the temperatures of the sensors mounted on the face.
Rationale: Sensor output varies with temperature (see section 4.6).
1.0.0.0 Requirements rationale