The invention relates to a four-rotor-wing indoor airship, which is designed by solving the technical problems of poor stability and flight control system complexity caused by the adoption of vector driving movement and posture height coupling of the existing indoor airship and particularly solving the technical problems of insufficient lifting force, static instability, poor safety, high noise, high cost and the like of an indoor special-shaped airship. The four-rotor-wing indoor airship comprises an airship capsule, four rotor wing assemblies and a hanging cabin, wherein the rotor wing assemblies are symmetrically distributed on the airship capsule, each rotor wing assembly comprises a rotor wing support arm, a rotor wing motor, a protecting ring and a propeller, the inner end of the rotor wing support arm is fixedly connected onto the airship capsule, the rotor wing motor is fixedly arranged at the outer side of the rotor wing support arm, the propeller is arranged on a rotating shaft of the rotor wing motor and is driven by the rotor wing motor, and the protecting ring surrounds the propeller and is fixedly arranged on the rotor wing motor. The four-rotor-wing indoor airship has the advantages that the structure is simple, the stability and the operability are high, the possibility for cooperatively completing various activities with people is provided, and because the stability enhancement control and flight principle similar to that of a four-rotor-wing helicopter is adopted, the four-rotor-wing indoor airship has the characteristic of adaptability to the insufficient lifting force and the static instability of a special-shaped airship structure. The four-rotor-wing indoor airship has the characteristics that the energy is saved, safety and reliability are realized, no pollution is caused, the noise is low, and the like, and the wide application of the indoor airship can be promoted.