ZONA proposes an innovative EGRM projectile design using body-conformal oblique wing/tails with smart-structure (actuator) control. This guided projectile can maintain optimal lift-to-drag ratio throughout its supersonic to subsonic flight phases and can achieve without rocket motor an extended range exceeding the maximum range required (63nm). With the guidance/nose cone section unaltered, the wing/tails fit conformally to the ERGM projectile skin structure with minimum impact to the remaining internal volume. The improved performance include: (a) large increase in the volume and warhead payload, (b) extended range; (c) increased mission flexibility by enhanced maneuverability; (d) reduced flight time; and (e) cost reduction. The proposed approach is to merge the outstanding aerodynamic characteristics of the oblique-wing/tails with smart structures for twist/camber control to achieve optimal lift-to-drag ratios throughout flight and enhanced maneuverability by adding direct lift control. Central in the smart-structure control system design is the use of ASTROS*(Automated Structural Optimization Systems, developed and improved by AFRL/ZONA) with other control algorithms. Other proposed tasks include smart-structure control system design, wing/tail smart-structures design integration, performance evaluation using a 6-DOF comprehensive simulation and to ingrate the simulation into the Phoenix Integration Corporation Model Center product.