The paper introduces a description of an automatic landing system for a Light Sport Aircraft (LSA) along with related concept and experimental validation by means of flight testing. The designed Linear Quadratic Regulator (LQR) which has been implemented on a digital autopilot was subjected to performance evaluations considering requirements inspired aerospace standard SAE AS94900. The autopilot's design robustness was tested on a LSA.
Light Sport Aircraft Auto-Land System
2019-09-01
3599388 byte
Conference paper
Electronic Resource
English
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