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Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Chapter 3 / Sensors<br />

_ _<br />

3.2 Generic Sensor Modelling<br />

Figure 3-1 captures the generic approach applied to sensor modelling.<br />

When a sensor is active its reference input is derived locally from reference<br />

state vector at the sensor update rate.<br />

A feature of this program and the AMIS is<br />

the way in which the sensors are isolated<br />

from the reference environment. Figure<br />

3-2 shows the sensors receiving data<br />

derived from the reference-state vector<br />

rather than the reference environment<br />

directly. In the AMIS the reference<br />

environment is defined by internal models,<br />

or by external data sources such as<br />

telemetry, HardWare-In-the-Loop (HWIL),<br />

and other simulations such as the Route<br />

Generation Program.<br />

Although this design approach leads to<br />

some inefficiency, it results in a singlethread<br />

modular structure. The interface<br />

between reference models and state vector<br />

can be fixed early in the design and data<br />

pre-processors put in place. Sensor models<br />

can then be developed in isolation without<br />

knowledge of the referenced model beyond<br />

the content of the reference state vector.<br />

Returning to Figure 3-1. The sensor<br />

dynamics and time dependent errors are<br />

modelled at the sensor reference rate,<br />

whether they are superimposed on the<br />

reference input or not, so as to avoid<br />

discontinuities in the output when toggling<br />

measurement availability or changing the<br />

output rate. The errors induced by<br />

Analogue-to-Digital Conversion (ADC)<br />

are an exception. These are applied at the<br />

output rate so as to respect the Zero-Order-<br />

Hold (ZOH) process on which they are<br />

based.<br />

The output interface model described in §0 can be characterised to represent<br />

system errors induced by various forms of digital interface between the<br />

sensors and state observers. The measurement errors are determined in each<br />

sensor module by comparing the reference input with the output from the<br />

digital interface.<br />

3.2-6<br />

NO<br />

YES<br />

SENSOR<br />

CONTROLLER<br />

SENSOR<br />

AVAILABLE<br />

YES<br />

SENSOR INPUT DERIVED<br />

FROM REFERENCE<br />

TARGET,<br />

MISSILE & SATELLITE<br />

DYNAMICS<br />

HIGH FREQUENCY<br />

ERROR DYNAMICS<br />

PERFECT<br />

SENSOR<br />

NO<br />

SUPERIMPOSE<br />

MEASUREMENT<br />

ERRORS AT<br />

TRANSMISSION RATE<br />

SENSOR TO<br />

FUSION FILTER<br />

INTERFACE<br />

NEXT SENSOR<br />

Figure 3-1<br />

Generic Sensor Error Model

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