Structural and functional insights into a novel pre-clinical-stage antibody targeting IL-17A for treatment of autoimmune diseases.

The pro-inflammatory cytokine interleukin-17A (IL-17A) is a key driver of multiple inflammatory and immune disorders. Therapeutic antibodies targeting IL-17A have been proven effective in treating patients with these diseases; however, large variations in clinical outcomes have been observed with different antibodies. In this study, we developed HB0017, a novel monoclonal antibody that targets human IL-17A. HB0017 specifically and strongly bound to human, cynomolgus monkey, and mouse IL-17A at the physiological interface with the IL-17A receptor. In human and monkey cells, HB0017 potently antagonized the functions of IL-17A through competitive binding. HB0017 functioned equivalently to that of clinically approved antibodies in terms of therapeutic efficacy for inflammatory disorders and psoriasis in a mouse model. The results indicate that HB0017 may be an alternative biological therapy for treating patients with inflammation and autoimmune diseases.

Ring Laser Gyro G-Sensitive Misalignment Calibration in Linear Vibration Environments.

The ring laser gyro (RLG) dither axis will bend and exhibit errors due to the specific forces acting on the instrument, which are known as g-sensitive misalignments of the gyros. The g-sensitive misalignments of the RLG triad will cause severe attitude error in vibration or maneuver environments where large-amplitude specific forces and angular rates coexist. However, g-sensitive misalignments are usually ignored when calibrating the strapdown inertial navigation system (SINS). This paper proposes a novel method to calibrate the g-sensitive misalignments of an RLG triad in linear vibration environments. With the SINS is attached to a linear vibration bench through outer rubber dampers, rocking of the SINS can occur when the linear vibration is performed on the SINS. Therefore, linear vibration environments can be created to simulate the harsh environment during aircraft flight. By analyzing the mathematical model of g-sensitive misalignments, the relationship between attitude errors and specific forces as well as angular rates is established, whereby a calibration scheme with approximately optimal observations is designed. Vibration experiments are conducted to calibrate g-sensitive misalignments of the RLG triad. Vibration tests also show that SINS velocity error decreases significantly after g-sensitive misalignments compensation.