Now showing items 11-20 of 2489
Unsteady Output-Based Adaptation Using Continuous-in-Time Adjoints
(American Institute of Aeronautics and Astronautics, 2017)
Parameter Governors for Coordinated Control of n-Spacecraft Formations
(American Institute of Aeronautics and Astronautics, 2017)
Design of a full time wing leveler system using tab driven aileron controls
(American Institute of Aeronautics and Astronautics, 1992)
Lambertian invariance and application to the problem of optimal fixed-time impulsive orbital transfer
(Elsevier, 1983)
To develop an efficient technique for the numerical solution of the Lambert problem, a new Lambertian invariant, the ratio of two invariable lengths, is proposed to replace the Gauss ratio of two areas as the main iterative ...
Zonal Wind Calculations from Mars Global Surveyor Accelerometer and Rate Data
(American Institute of Aeronautics and Astronautics, 2007)
Model calculations of the dayside ionosphere of Venus
(Elsevier, 1981)
Model calculations of the dayside ionosphere of Venus are presented. The coupled continuity and momentum equations were solved for O2+, O+, CO2+, C+, N+, He+, and H+ density distributions, which are compared with measurements ...
Education in the Crosscutting Sciences of Aerospace and Computing
(American Institute of Aeronautics and Astronautics, 2014-01-10)
Computation of Hypersonic Flows Using the Direct Simulation Monte Carlo Method
(Peer Reviewed, 2013)