Author Description

Pt. I. Attitude Dynamics I. Stability Relationships Between Gyrostats With Free, Constant Speed, And Speed Controlled Rotors (aas 81-100) / Tieshou Li, Richard W. Longman; Analytical Description Of The Attitude Motion Of A Spacecraft Containing Two Rotors (aas 81-101) / J.e. Cochran, Jr., P.h. Shu; Optimal Configurations For Dual-spin Satellites Subject To Gravitational Torques (aas 81-102) / Tieshou Li, Ruchard W. Longman; An Economical Series Solution Of Euler's Equations Of Motion, With Application To Space-probe Manoeuvres (aas 81-105) / H.l. Price; Analytical Approximation For Nutation Amplitude Resulting From Despin Through Unity Inertia Ratio (aas 81-103) Abstract / K.l. Lebstock, J.j. Mcennan, J.r. Murphy; Comments On The Leimanis Solution Of Self-excited Rigid Body (aas 81-104) Abstract / James M. Longuski -- Celestial Mechanics I. Short Period Elimination For The Tesseral Harmonics (aas 81-109) / S. Coffey, K.t. Alfriend; An Expression For The Nodal Period Correction Introduced By Earth Oblateness (j₂) (aas 81-110) / Robert C. Reynolds, Sean J. Mckenna; Ballistic Reentry Motion, Including Gravity: Constant Drag Coefficient Case (aas 81-111) / Michael E. Hough; The First-order Short-periodic Motion Of An Artificial Satellite Due To Third-body Perturbations (aas 81-106) Abstract / M.s. Slutsky, W.d. Mcclain; Long-term Prediction For High-altitude Orbits (aas 81-107) Abstract / Sean K. Collins, Paul J. Cefola; Computing High-altitude Satellite Orbits With The Halphen Method (aas 81-108) Abstract / R. Broucke, W. Presler; Perturbation Methods Based Upon Varying Action Integrals (aas 81-112) Abstract / Mahesh Rajan, John L. Junkins -- Mission Analysis For Solar System Exploration I. Interplanetary Navigation In The 1980's And 1990's (aas 81-113) / Lincoln J. Wood, James F. Jordan; Application Of Unconnected Phase Narrowband [delta]vlbi To Deep Space Navigation (aas 81-114) / J. Ellis, B. Moultrie, C.b. Smith; Optimization Of Extended Propulsion To