Autonomous navigation of generic Quadrocopter with minimum time trajectory planning and control

K. Bipin, Vishakh Duggal, K. Krishna
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引用次数: 10

Abstract

The challenges in generating minimum time trajectory and control for generic quadrocopter flying through sophisticated and unknown environment are explored in this paper. The proposed method uses convex programming technique to optimize polynomial splines, which are numerically stable for high-order including large number of segments and easily formulated for efficient computation. Moreover, exploiting the differential flatness of system, these polynomial trajectories encode the dynamics and constraints of the vehicle and decouple them from trajectory planning. The framework is fast enough to be performed in real time and results in solution which is close to time optimal. As control inputs are computed from the generated trajectory in each update, they are applicable to achieve closed-loop control similar to model predictive controller.
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通用四旋翼飞行器自主导航的最短时间轨迹规划与控制
探讨了通用四旋翼飞行器在复杂未知环境中飞行时的最短时间轨迹生成和控制问题。该方法采用凸规划技术对多项式样条曲线进行优化,该方法在高阶(包括大量线段)条件下具有数值稳定性,且易于表述,便于高效计算。此外,利用系统的微分平面性,这些多项式轨迹编码了飞行器的动力学和约束,并将它们与轨迹规划解耦。该框架速度快,可以实时执行,求解结果接近于时间最优。由于控制输入是根据每次更新生成的轨迹计算的,因此适用于实现类似于模型预测控制器的闭环控制。
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