TY - GEN
T1 - Impact time control with generalized look angle formulation under constraint
AU - Tekin, Raziye
AU - Erer, Koray S.
AU - Holzapfel, Florian
N1 - Publisher Copyright:
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - The nonlinear impact time control problem against stationary targets is investigated. The guidance law utilized in this paper is derived via shaping one of the fundamental states of the engagement. For that purpose, polynomial shaping of the look angle is considered. First, the boundary conditions of the engagement are introduced and the general form of the guidance law is presented. Afterwards, guidance gain determination for any order and the time domain solutions of the engagement are presented for the linearized kinematics. Later, the guidance law is modified for look angle constraint in an adaptive application scheme, which facilities closed loop application. The performance of the proposed guidance algorithm is demonstrated through simulations. In addition, a comparison study is held, whose results imply that the cubic polynomial is energy efficient for the look angle shaping.
AB - The nonlinear impact time control problem against stationary targets is investigated. The guidance law utilized in this paper is derived via shaping one of the fundamental states of the engagement. For that purpose, polynomial shaping of the look angle is considered. First, the boundary conditions of the engagement are introduced and the general form of the guidance law is presented. Afterwards, guidance gain determination for any order and the time domain solutions of the engagement are presented for the linearized kinematics. Later, the guidance law is modified for look angle constraint in an adaptive application scheme, which facilities closed loop application. The performance of the proposed guidance algorithm is demonstrated through simulations. In addition, a comparison study is held, whose results imply that the cubic polynomial is energy efficient for the look angle shaping.
UR - http://www.scopus.com/inward/record.url?scp=85083943940&partnerID=8YFLogxK
U2 - 10.2514/6.2019-1924
DO - 10.2514/6.2019-1924
M3 - Conference contribution
AN - SCOPUS:85083943940
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -