TY - JOUR
T1 - Derivative analysis and algorithm modification of the transverse- eccentricity-based Lambert's problem
AU - Wen, Changxuan
AU - Zhao, Yushan
AU - Shi, Peng
PY - 2013
Y1 - 2013
N2 - The classical Lambert's problem can be parameterized and solved through the transverse eccentricity component. A further study is conducted to calculate the derivative of the transverse-eccentricity-based Lambert's problem and to modify its algorithm. Results show that the derivative of a direct Lambert's problem is positive and continuous, which verifies that the transfer-time monotonically increases with the transverse eccentricity; however, the derivative of a multi-revolution Lambert's problem increases from negative to positive, indicating that the transfer-time decreases to the minimum firstly, and then increases to infinity. The original solution algorithm is promoted by introducing the analytic derivative. Numerical simulations for different cases show that, compared with the two existing transverse-eccentricity-based methods, the average computational time cost decreases by 65.5% and 39.8%, respectively.
AB - The classical Lambert's problem can be parameterized and solved through the transverse eccentricity component. A further study is conducted to calculate the derivative of the transverse-eccentricity-based Lambert's problem and to modify its algorithm. Results show that the derivative of a direct Lambert's problem is positive and continuous, which verifies that the transfer-time monotonically increases with the transverse eccentricity; however, the derivative of a multi-revolution Lambert's problem increases from negative to positive, indicating that the transfer-time decreases to the minimum firstly, and then increases to infinity. The original solution algorithm is promoted by introducing the analytic derivative. Numerical simulations for different cases show that, compared with the two existing transverse-eccentricity-based methods, the average computational time cost decreases by 65.5% and 39.8%, respectively.
UR - http://www.scopus.com/inward/record.url?scp=84898818792&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:84898818792
SN - 0065-3438
VL - 148
SP - 427
EP - 444
JO - Advances in the Astronautical Sciences
JF - Advances in the Astronautical Sciences
T2 - 23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013
Y2 - 10 February 2013 through 14 February 2013
ER -