Exploring the efficacy and safety of cannabidiol in individuals with epilepsy: an umbrella review of meta-analyses and systematic reviews.

Background: Epilepsy ranks among the most prevalent neurological conditions worldwide. Cannabidiol (CBD) has received authorization for epilepsy treatment, yet utilizing CBD is linked to a variety of adverse events (AEs). This umbrella review aims to explore risk and frequency of AEs in epilepsy patients undergoing treatment with CBD.

Cohort profile update: Tehran cardiometabolic genetic study.

The Tehran cardiometabolic genetic study (TCGS) is a large population-based cohort study that conducts periodic follow-ups. TCGS has created a comprehensive database comprising 20,367 participants born between 1911 and 2015 selected from four main ongoing studies in a family-based longitudinal framework. The study's primary goal is to identify the potential targets for prevention and intervention for non-communicable diseases that may develop in mid-life and late life.

Manifestations, Prevalence, Management and Outcome of Invasive in Post-Liver Transplant Patients.

Background: is a severe and fatal complication that causes infection in transplant recipients and patients with immunodeficiency syndrome, neutropenia, chronic granulomatosis, and hematologic malignancies. Invasive has been reported as one of the fungal infections with high mortality in transplant recipients. This study aimed to describe the manifestations, prevalence, management and outcome of invasive fungal infections in liver transplant patients.

Full quaternion based finite-time cascade attitude control approach via pulse modulation synthesis for a spacecraft.

In the aspect of further development of investigations in the area of spacecraft modeling and analysis of the control scheme, a new hybrid finite-time robust three-axis cascade attitude control approach is proposed via pulse modulation synthesis. The full quaternion based control approach proposed here is organized in association with both the inner and the outer closed loops. It is shown that the inner closed loop, which consists of the sliding mode finite-time control approach, the pulse width pulse frequency modulator, the control allocation and finally the dynamics of the spacecraft is realized to track the three-axis referenced commands of the angular velocities.