stephen whitmore
机构: Utah State University
每年引用次数
引用次数
引用: 3,036
H-指数: 32
I10-指数 : 81
出版物: 215
Air data position-error calibration using state reconstruction techniques
L. J. Ehernberger , T. J. Larson , S. A. Whitmore
8
1984
Flight and wind-tunnel comparisons of the inlet-airframe interaction of the F-15 airplane
D. Andriyich-Varda , L. D. Webb , S. A. Whitmore
2
1984
Formulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstruction
S. A. Whitmore
national aerospace and electronics conference 1 291 -298
5
1985
Radiation Heating Effects on Oxidizer-to-Fuel Ratio of Additively Manufactured Hybrid Rocket Fuels
S. A. Whitmore , S. Merkley
Journal of Propulsion and Power 35 ( 4) 863 -878
9
2019
Preliminary results from an airdata enhancement algorithm with application to high-angle-of-attack flight
TIMOTHY MOES , STEPHEN WHITMORE
29th Aerospace Sciences Meeting
10
1991
The effects of pressure sensor acoustics on airdata derived from a high-angle-of-attack flush airdata sensing (HI-FADS) system
STEPHEN WHITMORE , TIMOTHY MOES
29th Aerospace Sciences Meeting
33
1991
Formulaton of a general technique for predicting pneumatic attenuation errors in airborne pressure sensing devices
STEPHEN WHITMORE
4th Flight Test Conference
13
1988
Application of a flush airdata sensing system to a wing leading edge (LE-FADS)
STEPHEN WHITMORE , TIMOTHY MOES , MARK CZERNIEJEWSKI , DOUGLAS NICHOLS
31st Aerospace Sciences Meeting
12
1993
Failure detection and fault management techniques for flush airdata sensing systems
STEPHEN WHITMORE , TIMOTHY MOES , CORNELIUS LEONDES
30th Aerospace Sciences Meeting and Exhibit
7
1992
Preliminary results from a subsonic high-angle-of-attack flush airdata sensing (HI-FADS) system - Design, calibration, algorithm development, and flight test evaluation
STEPHEN WHITMORE , TIMOTHY MOES , TERRY LARSON
28th Aerospace Sciences Meeting
22
1990
Compensating for pneumatic distortion in pressure sensing devices
STEPHEN WHITMORE , CORNELIUS LEONDES
28th Aerospace Sciences Meeting
6
1990
Formulation and implementation of a practical algorithm for non-stationary adaptive state estimation
STEPHEN A. WHITMORE , CORNELIUS T. LEONDES
International Journal of Control 44 ( 3) 767 -775
2
1986
Parametric Study of Biconic Re-Entry Vehicles
Stephen A. Whitmore , Daniel W. Banks , Bryan Steele
2007
Preliminary airborne measurements for the SR-71 sonic boom propagation experiment
Edward A. Haering , Stephen A. Whitmore , L. J. Ehernberger
32
1995
Hydrocarbon-Seeded Ignition System for Small Spacecraft Thrusters Using Ionic Liquid Propellants
Daniel P. Merkley , Shannon D. Eilers , Stephen A. Whitmore , Terry L. Taylor
2
2013
Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack
Terry J. Larson , J. Blair Johnson , Paul M. Siemers , Stephen A. Whitmore
31
1987
High-angle-of-attack pneumatic lag and upwash corrections for a hemispherical flow direction sensor
Richard V. Deleo , Floyd W. Hagen , Terry J. Larson , Stephen A. Whitmore
2
1987
Experimental characterization of the effects of pneumatic tubing on unsteady pressure measurements
William T. Lindsey , Stephen A. Whitmore , Robert E. Curry , Glenn B. Gilyard
8
1990
Preliminary results from a subsonic high angle-of-attack flush airdata sensing (HI-FADS) system: Design, calibration, and flight test evaluation
Timothy R. Moes , Terry J. Larson , Stephen A. Whitmore
30
1990
Method for Reducing the Drag of Increasing Forebody Roughness Blunt-Based Vehicles by Adaptively Increasing Forebody Roughness
Timothy R. Moes , Edwin J. Saltzman , Stephen A. Whitmore , Kenneth W. Iliff
2005