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The automatic guidance of rotorcraft for obstacle avoidance in nap-of-the-earth flight is studied. The author considers a hierarchical breakdown of the guidance components to identify the functional requirements. These requirements and anticipated sensor capabilities lead to a preliminary guidance concept, which has been evaluated via computer simulations.< <ETX xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">></ETX>
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Victor Cheng (1990) studied this question.
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