32th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment

INVESTIGATIONS ON LANDING GEAR SHOCK ABSORBER ACTIVE FORCE CONTROL

Z. Skorupka¹, R. Harla¹; ¹Lukasiewicz Research Network - Institute of Aviation, Poland

Actively lowering the forces acting on aircraft fuselage touch down phase of the landing process is one key components of next generation landing gear optimization. In their paper authors present the physical principle of the process, means to achieve the forces/loads control, and their choice of control method for further laboratory testing.


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