During conceptual design, trajectory optimization is often performed using direct methods. This investigation illustrates that trajectory optimization and vehicle performance characterization can be rapidly performed by coupling indirect optimization, continuation, and symbolic manipulation. Examples illustrate that the historical challenges associated with indirect optimization methods can be overcome, enabling the rapid construction of high-quality solutions. In this design methodology, highly constrained optimal trajectories are rapidly constructed by traversing optimal manifolds of varying design problems throughout the continuation process. Presented as Paper 2011-6576 at the AIAA Atmospheric Flight Mechanics Conference, Portland, OR, 8-11 August 2011
Rapid Indirect Trajectory Optimization for Conceptual Design of Hypersonic Missions
Journal of spacecraft and rockets ; 52 , 1
2015
Aufsatz (Zeitschrift)
Englisch
Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
British Library Conference Proceedings | 2011
|Rapid Design Space Exploration for Conceptual Design of Hypersonic Missions
British Library Conference Proceedings | 2011
|