MINIMUM-TIME ROLL AROUND THE VELOCITY-VECTOR MANEUVER OF AIRCRAFT

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BAHRAMI MOHSEN; SADATI S.H.

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Journal Paper

Paper Information

Journal: ESTEGHLAL Year:2001 | Volume:20 | Issue:1 Page(s): 173-189

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Information Journal Paper

Title

MINIMUM-TIME ROLL AROUND THE VELOCITY-VECTOR MANEUVER OF AIRCRAFT

Author(s)

BAHRAMI MOHSEN | SADATI S.H. | Issue Writer Certificate

Keywords

MULTIPLE SHOOTING METHOD; MINIMUM TIME; THRUST-VECTORING; MANEUVERABILITY; AERODYNAMICSQ4

Abstract

New Page 1 this paper, some results are provided for minimum time roll about velocity vector maneuvering with thrust-vectoring and aerodynamic control in effect. The mathematical model for attitude motions of the aircraft is developed. First order necessary conditions for optimality using Pontryagen principle is applied, and the existence of an extreme family of solutions for the maneuver is shown. Multiple shooting method is used to obtain the numerical results. An estimate of maneuver time reduction resulting from thrust-vectoring is obtained.

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APA: Copy

BAHRAMI, MOHSEN, & SADATI, S.H.. (2001). MINIMUM-TIME ROLL AROUND THE VELOCITY-VECTOR MANEUVER OF AIRCRAFT. ESTEGHLAL, 20(1), 173-189. SID. https://sid.ir/paper/5891/en

Vancouver: Copy

BAHRAMI MOHSEN, SADATI S.H.. MINIMUM-TIME ROLL AROUND THE VELOCITY-VECTOR MANEUVER OF AIRCRAFT. ESTEGHLAL[Internet]. 2001;20(1):173-189. Available from: https://sid.ir/paper/5891/en

IEEE: Copy

MOHSEN BAHRAMI, and S.H. SADATI, “MINIMUM-TIME ROLL AROUND THE VELOCITY-VECTOR MANEUVER OF AIRCRAFT,” ESTEGHLAL, vol. 20, no. 1, pp. 173–189, 2001, [Online]. Available: https://sid.ir/paper/5891/en

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