Multiple-model control architecture for a quadrotor with constant unknown mass and inertia
نویسندگان
چکیده
منابع مشابه
A Digital Control Architecture for Quadrotor Aircraft
We show that the principal attitude and inertial dynamics of a quadrotor aircraft can be decomposed into a cascade of three passive and one interior conic subsystem such that a proportional digital feedback loop can effectively be applied to each subsystem in a nested manner. This proportional feedback architecture includes one saturation block nested between the attitude and inertial control s...
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ژورنال
عنوان ژورنال: Mechatronics
سال: 2021
ISSN: 0957-4158
DOI: 10.1016/j.mechatronics.2020.102455