The plant licorice is considered important plants as nutritionally and medically and economically, as a rich in phytochemical, vitamins and minerals, and being widely available, Research indicated the presence of many nutrients such as (proteins, Carbohydrates, vitamins and minerals) as well as presence of Glycyrrhizin which responsible of sweet taste, that allowing the possibility to use it as natural intensity sweetener with few calories in Sweetening of many food. This research is aimed to study the Stability of Glycyrrhizin toward the various manufacturing conditions such as (thermal treatment, pH of foods and microwaves), so three factorial experiments was implemented to find out the Stability as following: 100C° - 121C° - Microwaves [1150W] for 30-15-5 Min., respectively, under three levels of pH for each treatment 9.5 - 7.0 - 4.5 . It was found the high stability of Glycyrrhizin under 100C° - 121C° treatments under three levels of pH, as well as a significant increase in concentration at pH 9.5 - 4.5 at a temperature of 100C°. While the microwave treatment caused a significant decrease of Glycyrrhizin.
The effect of different thermal treatments and pH on the stability of a glycyrrhizin which Product from the licorice plant, Glycyrrhiza glabra L: The effect of different thermal treatments and pH on the stability of a glycyrrhizin which Product from the licorice plant, Glycyrrhiza glabra L
Glycyrrhizin
thermal treatments
sweetness
stability
microwaves.
Publication Date
Wed Dec 25 2019
Journal Name
Journal Of Engineering
Anti-Disturbance Compensator Design for Unmanned Aerial Vehicle
Quadrotor
Active disturbance rejection
UAV
Extended State observer
Hurwitz Stability
unmanned aerial vehicle
trajectory tracking
wind disturbance.
In this paper, an Anti-Disturbance Compensator is suggested for the stabilization of a 6-DoF quadrotor Unmanned Aerial vehicle (UAV) system, namely, the Improved Active Disturbance Rejection Control (IADRC). The proposed Control Scheme rejects the disturbances subjected to this system and eliminates the effect of the uncertainties that the quadrotor system exhibits. The complete nonlinear mathematical model of the 6-DoF quadrotor UAV system has been used to design the four ADRCs units for the attitude and altitude stabilization. Stability analysis has been demonstrated for the Linear Extended State Observer (LESO) of each IADRC unit and the overall closed-loop system using Hurwitz stability criterion. A minimization to a
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