This paper presents a novel configuration of flight vehicle with moving mass control. We focus on the development of the proposed control mechanism and investigate the feasibility of an equivalent experimental setup. First, the effect of the moving mass parameters on the control authority is investigated. Then, a control law based on immersion and invariance (I&I) theory is presented for the moving mass control system. In the design process, we select a first-order target system to reduce the difficulty of controller design. To deal with the coupling caused by the additional inertia moment, which is generated by the motion of the moving mass, the extended state observer (ESO) is designed. The proposed adaptive controller is simulated and tested on the experimental setup. Finally, the simulation results validate the quality of the proposed adaptive controller, which ensures a good performance in the novel configuration with internal moving mass.
Novel Moving Mass Flight Vehicle and Its Equivalent Experiment
Contributed by the Dynamic Systems Division of ASME for publication in the JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT,AND CONTROL. Manuscript received August 30, 2017; final manuscript received May 17, 2018; published online June 18, 2018. Assoc. Editor: Yongchun Fang.
- Views Icon Views
- Share Icon Share
- Cite Icon Cite
- Search Site
Li, J., Gao, C., Feng, T., and Jing, W. (June 18, 2018). "Novel Moving Mass Flight Vehicle and Its Equivalent Experiment." ASME. J. Dyn. Sys., Meas., Control. November 2018; 140(11): 111010. https://doi.org/10.1115/1.4040326
Download citation file:
- Ris (Zotero)
- Reference Manager