An approximate analytical solution of the multiple revolution Lambert's targeting problem is presented. The solution is obtained starting from Battin's optimum single-impulse transfer with a linear phasing correction and offers remarkable accuracy near minimum delta-V transfer conditions. Consequently, the method is useful for rapidly obtaining low delta-V solutions for interplanetary trajectory optimization. The solution is easy to program and non-iterative, which makes it ideal for GPU implementation. In addition, the method can be employed to provide a fast first guess solution for enhancing the convergence speed of an accurate numerical multi-revolution Lambert solver.

Approximate analytical solution of the multiple revolution Lambert's targeting problem

Gonzalo, JL
2016-01-01

Abstract

An approximate analytical solution of the multiple revolution Lambert's targeting problem is presented. The solution is obtained starting from Battin's optimum single-impulse transfer with a linear phasing correction and offers remarkable accuracy near minimum delta-V transfer conditions. Consequently, the method is useful for rapidly obtaining low delta-V solutions for interplanetary trajectory optimization. The solution is easy to program and non-iterative, which makes it ideal for GPU implementation. In addition, the method can be employed to provide a fast first guess solution for enhancing the convergence speed of an accurate numerical multi-revolution Lambert solver.
2016
Spaceflight Mechanics 2016
978-0-87703-633-3
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1221575
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