Lateral track control of UAVs using the sliding mode approach: From design to flight testing

Engineering

• Unmanned Aerial Vehicle 100%
• Sliding Mode 100%
• Flight Test 100%
• Straight Path 100%
• Ground Track 66%
• Test Result 33%
• Change Rate 33%
• Feedforward 33%
• Boundedness 33%
• Control Input 33%
• Circular Path 33%
• Roll Angle φ 33%
• Circular Arc 33%
• Curved Path 33%
• Crosswind 33%
• Flight Control 33%
• Lateral Plane 33%
• Lyapunov Function 33%
• Research Aircraft 33%