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5. Incremental Nonlinear Dynamic Inversion Control for Blended Wing Body Aircraft with Distributed Prop

Incremental Nonlinear Dynamic Inversion Control for Blended Wing Body Aircraft with Distributed Prop

来源 :第三届国际航空科学青年学者学术会议 | 被引量 : 0次 | 上传用户：william_wng

【出 处】

：

第三届国际航空科学青年学者学术会议

【发表日期】

：

2018年09期

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