Attitude Dynamics/Control of Dual-Body Spacecraft with Variable-Speed Control Moment Gyros
M. Romano, B. N. Agrawal
págs. 513-525
págs. 526-535
págs. 536-544
Flight Dynamics of the Boomerang, Part 1: Fundamental Analysis
G. Beppu, A. Azuma, H. Ishikawa
págs. 545-554
G. Beppu, H. Ishikawa
págs. 555-563
págs. 564-571
Minimum-Energy Output Transitions for Linear Discrete-Time Systems: Flexible Structure Applications
D. Iamratanakul
págs. 572-585
Dynamic Optimization Strategies for Three-Dimensional Conflict Resolution of Multiple Aircraft
A. U. Raghunathan
págs. 586-594
págs. 595-606
Tuning of Observer-Based Controllers
C. Cumer, C. Chiappa, D. Alazard, F. Delmond
págs. 607-615
Simulated Annealing for Missile Optimization: Developing Method and Formulation Techniques
O. Tekinalp
págs. 616-626
págs. 627-633
Missile Autopilot Design Using Discrete-Time Variable Structure Controller with Sliding Sector
A. A. Powly, M. S. Bhat
págs. 634-646
Computation of Controliability Regions for Unstable Aircraft Dynamics
M. G. Goman, M. N. Demenkov
págs. 647-656
Analytical Theory of Three-Degree-of-Freedom Aircraft Wing Rock
R. V. Ramnath, T. H. Go
págs. 657-664
págs. 665-677
Optimization of Variable-Specific-Impulse Interplanetary Trajectories
L. Casalino, G. Colasurdo
págs. 678-684
págs. 685-692
V. M. Guibout, D. J. Scheeres
págs. 693-704
págs. 705-709
Adaptive Output Feedback Control Methodology: Theory and Practical Implementation Aspects
A. J. Calise, N. Hovakimyan, M. Idan
págs. 710-714
págs. 715-719
págs. 720-723
Unified Algebraic Approach to Approximation of Lateral-Directional Modes and Departure Criteria
G. Mengali, F. Giulietti
págs. 724-727
Limit Cycles and Domain of Stability in Unsteady Aeroelastic System
S. N. Singh, S. Gujjula
págs. 728-732
Review of Formulas for Dynamic Analysis
K. Anderson
pág. 733
Review of Newton's Tyranny: The Suppressed Scientific Discoveries of Stephen Gray and John Flamsteed
M. Peck
págs. 734-735
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