Showing 1 - 7 results of 7 for search '', query time: 0.20s Refine Results
  1. 1
    An application of UAV attitude estimation using a low-cost inertial navigation system /

    An application of UAV attitude estimation using a low-cost inertial navigation system / by Eure, Kenneth W.

    Published 2013
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  2. 2
    Unit-sphere anisotropic multiaxial stochastic-strength model probability density distribution for the orientation of critical flaws /

    Unit-sphere anisotropic multiaxial stochastic-strength model probability density distribution for the orientation of critical flaws / by Nemeth, Noel N.

    Published 2013
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  3. 3
    ADDJUST : a view of the first 25 years /

    ADDJUST : a view of the first 25 years / by Nieberding, Joe, Williams, Craig H.

    Published 2015
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  4. 4
    Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display /

    Concepts for conformal and body-axis attitude information for spatial awareness presented in a helmet-mounted display / by Jones, Denise R., Abbott, Terence S., Burley, James R.

    Published 1993
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  5. 5
    Single axis attitude control and DC bus regulation with two flywheels /

    Single axis attitude control and DC bus regulation with two flywheels / by Kascak, Peter E.

    Published 2002
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  6. 6
    Polarized-interferometer feasibility study : final report /

    Polarized-interferometer feasibility study : final report / by Raab, Frederick H.

    Published 1983
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:
  7. 7
    Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing /

    Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wing / by Fink, Marvin P.

    Published 1969
    CONNECT
    Government Document Electronic eBook

    Save to List
    Saved in:

Search Tools: