Now showing items 1-2 of 2
Rudder Loss Recovery Autopilot System for a Small Fixed-Wing Aircraft
This paper presents an integrated way of development of an aircraft dynamic modeling including stability and control derivatives and ensuing autopilot design. Stability derivatives are calculated via an automated procedure ...
Moving Object Tracking using Simulated Motion Data
This paper presents the development of missile motion tracking using computer simulation and analyzes the results. In order to investigate the missile motion, simulated data and missile model is implemented in numerical ...