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Question: a tailless aircraft iscontrolled in pitch elevons each elevon is...

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A tailless aircraft is-controlled in pitch elevons. Each elevon is actuated by an inde- pendent power control unit. These units are so designed that if a failure occurs the affected el- evon is able to move until its(hinge moment is T0 A zero. Assuming the failure of one such unit, calculate the elevon angles that will give longitudinal trim of the aircraft whose details are given be- low:
Weight - Wing area S358m2 ho-0.15 Mo 850kN Speed7om/s EAS a2 = 0.95 -O Assume that each elevon contributes equally to a2 and to dao /or. 7failed9.61, 9.61°, η°perating -13.15°]
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