Description

The S4P flight control and navigation system is suitable for electric or fuel-powered small conventional fixed-wing, vertical take-off and landing fixed-wing, multi-rotor and other layout UAVs. It internally integrates a flight control computer and a high-precision, high-dynamic micro-integrated navigation system (GPS/ MINS), which can achieve one-button automatic takeoff, landing, hovering, circling, returning, altitude maintenance, parachute deployment, and autonomous cruising along a preset route. It supports cruise missile terminal guidance, networking and formation, supports high overload (maximum 100g) launch, and supports fixed and moving target attacks. The embedded digital aircraft model makes simulation flights easier and more convenient.
Vertical Take-Off and Landing Fixed-Wing Flight Control and Navigation System
Conventional Fixed-Wing (Hand Launch, Catapult Launch, Barrel  Launch,  Rocket  Assisted  Launch,  Parachute Deployment, Taxiing Takeoff and Landing) Flight Control and Navigation System
Quadrotor, Hexarotor, Octorotor, and Coaxial Dual-Rotor Flight Control and Navigation System