Harvey C
Department of Mechanical and Aerospace Engineering, University of California , Davis, CA 95616, USA.
J R Soc Interface. 2024 Apr;21(213):20230734. doi: 10.1098/rsif.2023.0734. Epub 2024 Apr 24.
Avian wing morphing allows dynamic, active control of complex flight manoeuvres. Previous linear time-invariant (LTI) models have quantified the effect of varying fixed wing configurations but the time-dependent effects of morphing between different configurations is not well understood. To fill this gap, I implemented a linear parameter-varying (LPV) model for morphing wing gull flight. This approach models the wing joint angles as scheduled parameters and accounts for nonlinear kinematic and gravitational effects while interpolating between LTI models at discrete trim points. With the resulting model, I investigated the longitudinal response associated with various joint extension trajectories. By optimizing the extension trajectory for four independent objectives (speed and pitch angle overshoot, speed rise time and pitch angle settling time), I found that the extension trajectory inherent to the gull wing does not guarantee an optimal response but may provide a sufficient response with a simpler mechanical implementation. Furthermore, the results indicated that gulls likely require extension speed feedback. This morphing LPV model provides insights into underlying control mechanisms, which may allow for avian-like flight in future highly manoeuvrable uncrewed aerial vehicles.
鸟类翅膀变形能够对复杂飞行机动进行动态、主动控制。以往的线性时不变(LTI)模型已经量化了不同固定机翼构型变化的影响,但对于不同构型之间变形的时间相关效应尚未得到充分理解。为了填补这一空白,我为变形翼海鸥飞行实现了一个线性参数变化(LPV)模型。这种方法将机翼关节角度建模为调度参数,并在离散配平点的LTI模型之间进行插值时考虑了非线性运动学和重力效应。利用所得模型,我研究了与各种关节伸展轨迹相关的纵向响应。通过针对四个独立目标(速度和俯仰角超调量、速度上升时间和俯仰角稳定时间)优化伸展轨迹,我发现海鸥翅膀固有的伸展轨迹并不能保证最优响应,但可能通过更简单的机械实现提供足够的响应。此外,结果表明海鸥可能需要伸展速度反馈。这种变形LPV模型为潜在的控制机制提供了见解,这可能使未来的高机动性无人飞行器实现类似鸟类的飞行。