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Stephen A. Whitmore

  • A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight programA base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
  • A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradientsA dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients
  • Air data position-error calibration using state reconstruction techniquesAir data position-error calibration using state reconstruction techniques
  • An optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pressure measurementsAn optimal deconvolution method for reconstructing pneumatically distorted near-field sonic boom pressure measurements
  • Compensating for pneumatic distortion in pressure sensing devicesCompensating for pneumatic distortion in pressure sensing devices
  • Design and calibration of the X-33 flush airdata sensing (FADS) systemDesign and calibration of the X-33 flush airdata sensing (FADS) system
  • Development of a closed-loop strap down attitude system for an ultrahigh altitude flight experimentDevelopment of a closed-loop strap down attitude system for an ultrahigh altitude flight experiment
  • Development of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) systemDevelopment of a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system
  • Failure detection and fault management techniques for a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) systemFailure detection and fault management techniques for a pneumatic high-angle-of-attack flush airdata sensing (HI-FADS) system
  • Formulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstructionFormulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstruction
  • In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) systemIn-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system
  • Measurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experimentMeasurement uncertainty and a feasibility study of a flush airdata system for a hypersonic flight experiment