An example can include a pod detachably coupled to a hull. At least one thrust generator can be fixed to the pod. A power source can be mounted to the pod and slideable fore and aft. A power source actuator can be coupled between the pod and the power source to translate the location of the power source with respect to the pod. A sensor can be coupled to the pod to detect a pitch of the hull and provide a pitch signal. A controller can be coupled to one or more of the power source, the power source actuator, the first and second thrust generators and the sensor. The controller can maintain a pitch of the hull by translating the power source within the pod in association with the pitch signal.


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    Titel :

    Airship pitch trim and directional control system


    Beteiligte:

    Erscheinungsdatum :

    2016-05-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft



    AIRSHIP PITCH TRIM AND DIRECTIONAL CONTROL SYSTEM

    SMITH MICHAEL SCOTT / SCOTT RANDY E | Europäisches Patentamt | 2016

    Freier Zugriff

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    SMITH MICHAEL SCOTT / SCOTT RANDY E | Europäisches Patentamt | 2017

    Freier Zugriff

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    Airship trim and stability analysis using bifurcation techniques

    Tiwari, Anshul / Vora, Anuj / Sinha, Nandan Kumar | IEEE | 2016


    Directional control of an advanced airship

    Nagabhushan, Bellur L. / Tan, Swee B. | AIAA | 1996