Deprecated: $wgMWOAuthSharedUserIDs=false is deprecated, set $wgMWOAuthSharedUserIDs=true, $wgMWOAuthSharedUserSource='local' instead [Called from MediaWiki\HookContainer\HookContainer::run in /var/www/html/w/includes/HookContainer/HookContainer.php at line 135] in /var/www/html/w/includes/Debug/MWDebug.php on line 372
scientific article; zbMATH DE number 745844 - MaRDI portal

scientific article; zbMATH DE number 745844

From MaRDI portal
Publication:4763796

zbMath0815.70002MaRDI QIDQ4763796

John E. Prussing, Bruce A. Conway

Publication date: 20 April 1995


Title: zbMATH Open Web Interface contents unavailable due to conflicting licenses.



Related Items (23)

Measuring the constrained reachability in quantum Markov chainsThe equations of relative motion in the orbital reference frameExistence of periodic motions of a tether trailing satelliteBallistic missile trajectory prediction using a state transition matrixA new procedure for the solution of the classical problem of minimal orbit determination from three lines of sightSymmetry properties of optimal relative orbit trajectoriesThe eleventh motion constant of the two-body problemComputing a Satellite Orbit From PhotographsSparse-grid quadrature nonlinear filteringMeasurement-based perturbation theory and differential equation parameter estimation with applications to satellite gravimetryA closed-form solution to the minimum \(\Delta V_{\text{tot}}^{2}\) Lambert's problemRobust tracking control for rendezvous in near-circular orbitsOptimal starting conditions for the rendezvous maneuver. I: Optimal control approachOptimal starting conditions for the rendezvous maneuver. II: Mathematical programming approachOptimal trajectories for spacecraft rendezvousGuidance trajectories for spacecraft rendezvousPosition and velocity perturbations for the determination of geopotential from space geodetic measurementsNumerical solution of orbital combat games involving missiles and spacecraftReconstruction of the Fourier expansion of inputs of linear time-varying systemsNovel spaceways for reaching the Moon: An assessment for explorationOptimal space trajectories with multiple coast arcs using modified equinoctial elementsApproximating orbits in a rotating gravity field with oblateness and ellipticity perturbationsA tutorial history of least squares with applications to astronomy and geodesy




This page was built for publication: