Stall Recovery Guidance Algorithms Based on Constrained Control Approaches

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

Aircraft loss-of-control, in particular approach to stall or fully developed stall, is a major factor contributing to aircraft safety risks, which emphasizes the need to develop algorithms that are capable of assisting the pilots to identify the problem and providing guidance to recover the aircraft. In this paper we present several stall recovery guidance algorithms, which are implemented in the background without interfering with flight control system and altering the pilot's actions. They are using input and state constrained control methods to generate guidance signals, which are provided to the pilot in the form of visual cues. It is the pilot's decision to follow these signals. The algorithms are validated in the pilot-in-the loop medium fidelity simulation experiment.

Authors

• Stepanyan, Vahram University Affiliated Research Center (Calif. Univ. Santa Cruz)
• Krishnakumar, Kalmanje NASA Ames Research Center
• Kaneshige, John NASA Ames Research Center
• Acosta, Diana NASA Ames Research Center

Keywords

• Aircraft stall
• Pilot visual cueing
• Recovery guidance algorithm