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Abstract

The use of thrust vectoring technologies for performing extremely short takeoff and landing (ESTOL) operations was recently successfully demonstrated in a series of flight experiments involving an X-31 aircraft.

The study presented herein builds on these ESTOL developments. More specifically, the main goal of the present study is to shape high angle-of-attack approach trajectories in such a way that starting at a given altitude and speed, the down-range distance to the runway threshold is minimized. In other words, the steepest approach possible is explored.

The approach-to-landing problem is formulated as an optimal control problem and solved numerically, using a rigid-body model of a thrust-vectored version of an F-16 fighter aircraft. The employed numerical method, collocation with non-linear programming, proves well suited for solving this problem.

Keywords

extremely short takeoff and landing (ESTOL)trajectory optimization thrust vectoring

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References

Young

X31 VECTOR Program Summary. In AIAA Guidance, Navigation, and Control Conference, 2004, Providence, Rhode Island).

Selmon

J. R.

White

S. N.

Sheen

J. H.

Bass

D. I.

Miranda

High angle of attack autonomous landing using the X-31A aircraft. In AIAA Guidance, Navigation, and Control Conference, 2001, (Montreal, Canada).

O'Rourke

M. J.

Ralston

J. N.

Bell

J. W.

PC-based simulation of the F-16/MATV. In AIAA Modeling and Simulation Technologies Conference, 1997, (New Orleans, Louisiana).

Komduur

H. J.

Visser

H. G.

Optimization of pitch reversal standard agility comparison maneuvers. J. Quid. Contr. Dyn., 2002, 25 (4), 693–702.

Morelli

E. A.

Global nonlinear parametric modeling with application to F-16 aerodynamics. In American Control Conference, 1998, Vol. 2, pp. 997–1001 (Philadelphia, USA).

Hoak

D. E.

Carlson

M. W.

Finck

R. D.

USAF stability and control DATCOM. Wright-Patterson Air Force Base, OH, 1970.

Stevens

B. L.

Lewis

F. L.

Aircraft control and simulation, 1992 (Wiley-Interscience, New York).

Visser

H. G.

Optimization of high angle-of-attack approach and landing trajectories. In 24th Congress of the Aeronautical Sciences, 2004 (Yokohama, Japan).

Friehmelt

Thrust vectoring and tailless aircraft design - review and outlook. In AIAA Atmospheric Flight Mechanics Conference, 1996 (San Diego, USA).

10.

Hargraves

C. R.

Paris

S. W.

Direct trajectory optimization using nonlinear programming and collocation. J. Quid. Contr. Dyn., 1987, 10 (4), 780–785.

11.

Seywald

Kumar

EZopt: An optimal control toolkit, 1997 (Analytical Mechanics Associates, Inc., Hampton, VA).

12.

Ruijgrok

G. J. J.

Elements of airplane performance, 1990 Delft University Press, Delft, The Netherlands).

Optimization of High Angle-of-Attack Approach to Landing Trajectories

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