All Stories

  1. Design of Adaptive Sliding Mode Control for Uncertain Thrust Vectored Airship
  2. Direct Methodology for Constrained System Analysis with Applications to Aircraft Dynamics
  3. Analysis and modelling of septic shock microarray data using Singular Value Decomposition
  4. Quasi-periodic dynamics of a high angle of attack aircraft
  5. Airship trim and stability analysis using bifurcation techniques
  6. Design and Simulation of Autopilot Control System for Stratospheric Airship
  7. A New Guidance Law for the Defense Missile of Nonmaneuverable Aircraft
  8. Aircraft Design Using Constrained Bifurcation and Continuation Method
  9. The Target Guarding Problem Revisited: Some Interesting Revelations
  10. Key factors that affect the performance of flares against a heat-seeking air-to-air missile
  11. Accessible Regions for Controlled Aircraft Maneuvering
  12. A Simple, Correct Pedagogical Presentation of Airplane Lateral-Directional Dynamics
  13. A Simple, Correct Pedagogical Presentation of Airplane Longitudinal Dynamics
  14. Aircraft Design Using Constrained Bifurcation and Continuation Method
  15. A sliding mode controller for aircraft simulated entry into spin
  16. Aircraft Maneuver Design Using Bifurcation Analysis and Sliding Mode Control Techniques
  17. Autorotational Spin Evolving Towards Chaos
  18. Aircraft Maneuver Design using Bifurcation Analysis and Nonlinear Control Techniques
  19. Aircraft Spin Recovery Using a Sliding-Mode Controller
  20. Computational Bifurcation Analysis of Multiparameter Dynamical Systems
  21. Wind-excited overhead transmission lines: Estimation of connection stresses at junctions
  22. Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art
  23. Automated gain scheduling using continuation techniques
  24. Automated Gain Scheduling for Level Flight Stability Augmentation Using Continuation Techniques
  25. Maximum Steady Roll Rate in Zero-Sideslip Roll Maneuvers of Aircraft
  26. Applications of Bifurcation Methods to F-181HARV Open-loop Dynamics in Landing Configuration