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The design and implementation of an autonomous guidance system requires knowledge and an understanding of a wide range of technologies, from the physical dynamics of the vehicle (including mechanical and structural properties) to the accuracies and inaccuracies of the sensors used to guide the vehicle. At the simplest level a guidance system has: - A sensor to generate measurements. - A guidance law to convert the measurements into a requirement (usually a requirement on the acceleration of the vehicle). - A dynamical model/transfer function to convert the requirement into a desired control/command. - A control system to minimise the difference between the desired control and the actual control achieved.
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Maximum speed -Pro craft The standard approach for prop-driven aircraft is to assume that engine and propeller together produce a power (as opposed to thrust) output that is ind
Causes of unbalance Unbalance may be caused by a variety of factors occurring singly or in combination with others. These factors include:- a) Eccentricity Eccentricity
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Smoke control system: Where smoke control is installed in a building it is usual for there to also be sprinkler protection to the building and its contents. This is necessary
calculate the workdone by a system which contains 10kg of this gas expanding from 1m^3 at temperature of 293k, use the values a=15.7*10Nm^4, b=1.07*10^-2m^3 , R=0.278KJ/Kg-k.
Consider 1:1 stoichiometric polymerisation of 1,4-diaminobutane with sebacoyl chloride. (a) Write down a balanced chemical equation for the polymerization (b) Name the polymer fo
Question: (a) OFDM signals have a higher PAPR that signal carrier signals do. Describe (i) Why this is so and what is the impact on radio transmission systems? (ii) How
Suggest an example of a decision from your own experience which you feel is best treated as a decision without probabilities. What principle of choice would seem appropriate?
Inlet duct arrangement in Aircraft Engine: Wherever the APU is located, ducting will be required to bring air to the APU inlet. In figure 18.9. we can see that the inlet duct
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