In this paper, an approximate solution of sensitivity matrix of required velocity with final velocity constraint is derived using a piecewise linear gravity assumption. The total flight time is also fixed for the problem. Simulation results show the accuracy of the method. Increasing the midway points for linearization, increases the accuracy of the solution, which this, in turn, depends on the total flight time.
Jalali Naini,S. (2012). Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption. (e51619). Journal of Aerospace Science and Technology, 9(2), e51619
MLA
Jalali Naini,S. . "Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption" .e51619 , Journal of Aerospace Science and Technology, 9, 2, 2012, e51619.
HARVARD
Jalali Naini S. (2012). 'Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption', Journal of Aerospace Science and Technology, 9(2), e51619.
CHICAGO
S. Jalali Naini, "Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption," Journal of Aerospace Science and Technology, 9 2 (2012): e51619,
VANCOUVER
Jalali Naini S. Approximate Solution of Sensitivity Matrix of Required Velocity Using Piecewise Linear Gravity Assumption. Journal of Aerospace Science and Technology, 2012; 9(2): e51619.
