Due to mass constraints, the Orion Command Module landing attention system requires that the capsule be oriented in a specific direction with respect to the horizontal surface-relative velocity (Heading) at touchdown in order to keep crew and vehicle loads within specifications. These constraints apply to both land and water landings. In fact, water landings are even more constrained with the addition of impact angle requirements necessary to slice through the water. There are two primary challenges with achieving this touchdown orientation: 1. Navigation knowledge of velocity (needed to determine Heading) with and without GPS, including the effects of the Heading angle itself becoming undefined as horizontal velocity decreases, and 2. Controlling to the desired orientation in the presences of chute torque and wind gusts that may change the Heading just prior to touchdown. This paper will discuss the design and performance of the current Orion navigation and control system used to achieve the desired orientation at touchdown.


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    Titel :

    Challenges of Roll Orientation with Respect to Vehicle Heading at Touchdown for the Orion Command Module


    Beteiligte:
    Gay, Robert S. (Autor:in) / Bihari, Brian D. (Autor:in)

    Kongress:

    31st Annual AAS Guidance and Control Conference ; 2008 ; Breckenridge, CO, United States


    Erscheinungsdatum :

    01.02.2008


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Challenges of Roll Orientation with Respect to Vehicle Heading at Touchdown for the Orion Command Module (AAS 08-068)

    Gay, R.S. / Bihari, B.D. / American Astronautical Society | British Library Conference Proceedings | 2008


    Orion Touchdown Heading Control

    Kane, Mark A. | NTRS | 2010


    Orion Touchdown Heading Control

    M. A. Kane | NTIS | 2010