Guidance and control system of missiles and space vehicles is discussed which consists of two control loops; inner-control loop (autopilot) on-board of vehicle ensures parallel orientation of its roll-, pitch-, and yaw-axes toward fixed reference system; ground-installed outer control loop (guidance loop) guides vehicle and provides necessary correcting orders; interference on autopilot of such factors as aerodynamic forces, structural vibrations, fuel slashing, staging, and noise can be reduced by means of precise control system as well as appropriate structural design. (n 16 June (I) p 701-6)


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    Titel :

    Guidance of rockets


    Weitere Titelangaben:

    Steuerung der Raketen


    Beteiligte:
    Klamka, N. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Homing Guidance of Rockets

    V. I. Kurkotkin / V. L. Sterligov | NTIS | 1964


    Optimal Guidance of Rockets

    Tewari, Ashish | Wiley | 2011


    Solid-state guidance for Able-series rockets

    King, R.E. / Low, H. | Engineering Index Backfile | 1960


    Operational Atmospheric Landing Guidance for Reusable Rockets

    Sagliano, Marco / Farì, Stefano / Macés Hernández, José et al. | AIAA | 2025