AERO-MTECH-05-001




Development of a control system for remotely controlled non-rigid airship
Devendra Khitoliya, M.Tech, 05, 69 pp.
Department of Aerospace Engineering
Indian Institute of Technology Bombay, Powai, Mumbai 400 076.
Supervisor(s): R. K. Pant

An airship is a lighter than air vehicle that derives its lift mainly from buoyancy. An airship is considered to be the most capable vehicle for long endurance flight at low speeds, for applications such as advertisement, scientific exploration, and aerial surveillance. The most common type of airship currently in use is the non-rigid airship, also called as “blimp”. An airship is a highly non-linear and complex system; hence modeling its dynamics poses several challenges, compared to a heavier-than-air aircraft. Due to its buoyant nature, very large volume and considerable change in the center of gravity location during operation, added or virtual mass terms assume importance in its dynamic modeling and inertia properties. This study covers literature survey related to the modeling of airship dynamics, stability, control and its simulation. Some issues related to the operation of non-rigid airships are highlighted. Non-linear equations of motion are derived from the standard equations of motion of a rigid body with 6 degrees of freedom. The dynamic modeling includes the effects of virtual mass and inertia. A procedure for estimation of various airship related parameters required for the simulation of its dynamics is outlined. A linear PID controller is designed for the decoupled longitudinal and lateral-directional motion of an airship. The behavior of an airship can be determined by the simulation of this non-linear model for different cases of inputs. Finally, the linear controller is applied to non-linear dynamic model for a case of tracking of forward velocity at various speeds, at a given altitude. The linear PID controller seems to work well with the non-linear model, as it gives the limiting overshoot. The time response of the PID controller for forward velocity also matched quite well with the published results using an autopilot system. ��