October 5, 2026 B. G. Doerr, R. Linares, C. D. Petersen “Spacecraft Attitude Control using Path Integral Method via Riemann Manifold Hamiltonian Monte Carlo” Space Flight Mechanics Meeting [Conference] . (2018): . Print. Share this . (2018): . Print."] Related Stories See all news The next generation’s guide to the new space economy Coordinated satellite, aircraft, and ground-based observations of a large transient methane release See all news
