The Flight Dynamics Simulation Of Carrier-Based Aircraft

This thesis is based on the flight mechanics of Carrier-Based Aircraft's landing. With the increase of China's comprehensive national strength, more attention is paid on the China's maritime security issues. Aircraft carrier, as the traffic lines of seas and the maritime lifeline, its development is conducive to defense our waters, while Carrier-Based Aircraft is one of the most important weapons on the aircraft carrier. Carrier aircraft carrier always be accompanied by the generation, development, is developing rapidly, and the aircraft carrier super capacity is the most important reflect, its main task is to escort, seizing fleet sea or air, sea coast, attack enemy fleet and onshore goals, support landing and resistance to landing operations etc. Carrier-based aircraft landing on aircraft carriers is very difficult and extremely dangerous, known as accident prone stage, so improving carrier-based aircraft landing safety has a big significance in operational effectiveness of the protection of an aircraft carrier.This thesis is mainly about Carrier-Based Aircraft's flight fhase landing, not involved the landing after. Basing on the flight mechanics and combining the analysis of the aerodynamic force and aerodynamic moment when the aircraft flying, derivate the locus equation of the aircraft. Regarded Su-33 aircraft as template, simulate the process of its carrier landing. Because of the aerodynamic force or some else's influence, flight attitude should be adjusted properly when its landing. Through the adjustment of the elevator, the aircraft carrier landing flight attitude can be described in a landing trajectory in this study.In this study, simulating Carrier-Based Aircraft's landing on the flight path has some reference value in practical engineering calculations, but there are still many shortcomings to correct in the furthermore study.