Abstract-In this paper, exponentially stable non-linear observers for estimation of position, velocity, specific force, attitude and gyro bias of a fixed-wing unmanned aerial vehicle (UAV) are proposed. The sensor suite consists of an Inertial Measurement Unit (IMU), a global navigation satellite system (GNSS) receiver, a camera, an altimeter, and, possibly, auxiliary roll and pitch measurements. A first observer is designed making use of all the named sensors and is proven to be globally exponentially stable (GES). Subsequently, the auxiliary roll and pitch measurements are removed and replaced by an additional feedback loop from the estimated attitude, and the new observer is analysed and proven to be uniformly locally exponentially stable (ULES). An optical flow algorithm is used to calculate the UAV velocity based on the camera images, which is used as a measurement of the body-fixed velocity in the attitude observer. The performance of the observers is tested offline on simulated and experimental data.