They can very the sweep of a straight wing for optimal configuration throughout the design speeds. (they have good low-speed landing and takeoff performance while being able to rotate the wing for high L/D ratios at supersonic flight. The Lift dependent wave drag is 1/4 less than conventional variable-sweep aircraft and the volume-dependent wave drag is 1/16 less than conventional variable-sweep aircraft. The wing structure itself is simple.
[[Challenges of Oblique Wing Aircraft]]
[[Sliding Mode Controller]] -had a high closed-loop overshoot for near-space OWA
Oblique Wing Aircraft Moment Equations
[[Oblique Wing Aircraft Nonlinear Equations of Motion]]
[[Oblique Wing Aircraft Control Weighting]]
[[Oblique Wing Ideal Control Responses]] – used with NDI
[[Oblique Wing Outer-loop Equations]]
[[Oblique Wing Inner Loop Equations]]
Sources
- [1] L. Wang, Z. Xu, and T. Yue, “Dynamic characteristics analysis and flight control design for oblique wing aircraft,” Chinese Journal of Aeronautics, vol. 29, no. 6, pp. 1664–1672, Dec. 2016, doi: 10.1016/j.cja.2016.10.010.
Backlinks
[[Command Augmentation System]]
Dynamic Inversion Control Law Structure
F-22 Flight Control System
[[Inertial Coupling]]
LQR Controller
[[Phugoid]]
[[Pseudo Controls]]
[[Short-Period]]
[[Wave Drag]]