Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
863600 | Procedia Engineering | 2011 | 15 Pages |
Abstract
In terms of safety for landing taxiing control of high-speed unmanned air vechicles (UAVs), key safety-critical factors were first. A generic taxiing control logic was put forward, incorporating the concerned factors. For further verification, a nonlinear mathematic model was deduced with high accuracy for ground motion simulation, incorporating the characteristics of undercarriages, brake, nose wheel steering and runway condition. Simulations show that the control logic works well and provides sAttention:ufficient safety assurance in even extreme situations experienced.
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