Atmospheric turbulence models are necessary for the design of both inlet/engine and flight controls, as well as for studying integrated couplings between the propulsion and the vehicle structural dynamics for supersonic vehicles. Models based on the Kolmogorov spectrum have been previously utilized to model atmospheric turbulence. In this paper, a more accurate model is developed in its representative fractional order form, typical of atmospheric disturbances. This is accomplished by first scaling the Kolmogorov spectral to convert them into finite energy von Karman forms. Then a generalized formulation is developed in frequency domain for these scale models that approximates the fractional order with the products of first order transfer functions. Given the parameters describing the conditions of atmospheric disturbances and utilizing the derived formulations, the objective is to directly compute the transfer functions that describe these disturbances for acoustic velocity, temperature, pressure, and density. Utilizing these computed transfer functions and choosing the disturbance frequencies of interest, time domain simulations of these representative atmospheric turbulences can be developed. These disturbance representations are then used to first develop considerations for disturbance rejection specifications for the design of the propulsion control system and then to evaluate the closed-loop performance.

References

1.
Nastrom
,
G. D.
, and
Gage
,
K. S.
, 1985, “
A Climatology of Atmospheric Wavenumber Spectra of Wind and Temperature Observed by Commercial Aircraft
,”
J. Atmos. Sci.
,
42
(
9
), pp.
950
960
.
2.
Fairall
,
C. W.
,
White
,
A. B.
, and
Thompson
,
D. W.
, 1991, “
A Stochastic Model of Gravity-Wave-Induced Clear-Air Turbulence
,”
J. Atmos. Sci.
,
48
(
15
),
1771
1790
.
3.
Tatarski
,
V. I.
, 1961,
Wave Propagation in a Turbulent Medium
,
McGraw-Hill
,
Toronto, Canada
.
4.
Kolmogorov
,
A. N.
, 1941, “
Dissipation of Energy in the Locally Isotropic Turbulence
,”
C. R. (Dokl.) Acad. Sci. URSS
,
32
, pp.
16
18
.
5.
Kolmogorov
,
A. N.
, 1941, “
The Local Structure of Turbulence in Incompressible Viscous Fluid for Very Large Reynold’s Numbers
,”
C. R. (Dokl.) Acad. Sci. URSS
,
30
, pp.
301
305
.
6.
Houbolt
,
J. C.
,
Steiner
,
R.
, and
Pratt
,
K. G.
, 1964, “
Dynamic Response of Airplanes to Atmospheric Turbulence Including Flight Data on Input Response
,” NASA Technical Report No. R–199.
7.
Tank
,
W. G.
, 1994, “
Atmospheric Disturbance Environmental Definition
,” NASA CR–195315.
8.
Hoblit
,
F. M.
, 1988,
Gust Loads on Aircraft: Concepts and Applications
,
AIAA Education Series
,
Washington, DC
.
9.
Kopasakis
,
G.
, 2010, “
Atmospheric Turbulence Modeling for Aero Vehicles—Fractional Order Fits
,” NASA/TM-2010-216962.
10.
Tank
,
W. G.
, and
Gillis
,
J.
, 1996, “
Atmospheric Disturbance Models for Linear and Nonlinear System Response Analysis
,” AIAA 34th Aerospace Sciences Meeting and Exhibit, Reno, NV.
11.
McMinn
,
J. D.
, 1997, “
Extension of a Kolmogorov Atmospheric Turbulence Model for Time-Based Simulation Implementation
,” AIAA Guidance Navigation and Control Conference, AIAA–97–3532, New Orleans, LA, Aug. 11–13.
12.
Johnson
,
D. L.
, 1993, “
Terrestrial Environment (Climatic) Criteria for Use in Aerospace Vehicle Development
,” 1993 Revision, NASA TM–4511.
13.
Soreide
,
D. C.
, and
Tank
,
W. G.
, “
Proposed Model of the Atmosphere for the High Speed Civil Transport Program
,” (to be published).
14.
Ashun
,
U.
,
Merchant
,
A.
,
Paduano
,
J.
, and
Drela
,
M.
, 2003, “
Design of an Actively Stabilized, Near-Isentropic Supersonic Inlet
,” AIAA Computational Fluid Dynamics Conference, AIAA–2003–4069 Orlando, FL, 23–26 June.
15.
Kopasakis
,
G.
, and
Connolly
,
J. W.
, 2009, “
Shock Positioning Controls Design for a Supersonic Inlet
,” AIAA 45th Joint Propulsion Conference, AIAA–2009–5117, Denver, CO, Aug. 2–5.
16.
Kopasakis
,
G.
, 2007, “
Feedback Control Systems Loop Shaping Design With Practical Considerations
,” NASA/TM—2007-215007.
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