From Theory to Flight: Design and Application of Pitch Rate Control Augmentation Systems

Ramona Devi

Abstract: Control Augmentation Systems (CAS) are indispensable components of high-performance military aircraft that provide pilots with the means to optimize control, maneuverability, and agility during manual flight operations. This paper focuses on the design and implementation of Pitch Rate Control Augmentation Systems as an essential subset of CAS. Using the example of an F-16 aircraft, this paper explores the design process, control parameters, and feedback gains involved in developing an effective pitch-rate CAS. The results highlight the impact of various design choices on system behavior, demonstrating the importance of fine-tuning CAS for specific mission requirements and flying conditions.

Keywords: pitch rate control, CAS, flight, control, autopilot