FixedWingLib CGF for VR-Forces
"FixedWingLib CGF for VR-Forces" allows users and developers to use high fidelity FixedWingLib CGF aircraft models and maneuvers in VR-Forces.
"FixedWingLib CGF for VR-Forces" can simulate many real-world fixed wing aircraft scenarios:
- Formation flight
- Weaving
- Terrain following
- Realistic ground taxi, take off and landing
- Air combat maneuvers ( Pursuit, Immelmann turn and many more )
- VTOL take off, hover and landing
Applications
Air Combat Simulations
Aerial Refueling Simulations
UAV Operator Trainers
UAV Pilot Trainers
Embedded Training
Full Mission Simulators
Engineering Simulations
Hardware-in-the-loop Simulations
Air Combat Simulations
Aerial Refueling Simulations
UAV Operator Trainers
UAV Pilot Trainers
Embedded Training
Full Mission Simulators
Engineering Simulations
Hardware-in-the-loop Simulations
Core Features
- Supports all VR-Forces fixed-wing aircraft tasks and set data requests.
- High fidelity flight dynamics for standard VR-Forces tasks
- High fidelity joystick flight
- Additional Tasks: VTOL take off, hover and landing
- Additional Set Data Requests: weaving, terrain following, dynamic flight limits
- Allows specification of aircraft agility with g-load, roll rate and vertical climb speed during simulation. This feature allows switching to high-g defensive and offsensive maneuvers during engagement.
- FixedWingLib CGF features
- 6 DOF Physics Based Flight Dynamics Models
- Navigational maneuvers
- Joystick flight with direct aileron, elevator, throttle and air brake control
- Extensible controllers to create new maneuvers
- More
- Combat Maneuvers Library features
- Air combat maneuvers (such as S-turn, Scissors, Low and High Yoyo and more)
- Close air support maneuvers (such as dive bombing)
- More
Dynamics Flight Limits
FixedWingLib CGF allows changes to the flight limits during simulation. By adjusting parameters such as maximum G load, desired roll speed or desired vertical speed, users can specify the aggressiveness of the maneuvers. These parameters immediately influence aircraft performance. The limits can be adjusted as often as necessary.




