Proceedings ArticleDOI
Guidance, Navigation and Control Without Gyros: A Gun-Launched Munition Concept
Reads0
Chats0
Citations
More filters
Proceedings ArticleDOI
Inertial sensor arrays — A literature review
John-Olof Nilsson,Isaac Skog +1 more
TL;DR: A brief summary and literature review on the topic of inertial sensor arrays is provided and an outlook on the main research challenges and opportunities related to inertial Sensor arrays is given.
Journal ArticleDOI
Effective Use of Magnetometer Feedback for Smart Projectile Applications
TL;DR: In this article, the effect of spin-induced magnetic field distortion is discussed, with particular attention to its implications for magnetometer-based orientation estimation, and a comprehensive algorithm is built as a coupled set of Extended Kalman filters.
Proceedings ArticleDOI
Assessment of a GPS Guided Spinning Projectile Using an Accelerometer -Only IMU
TL;DR: In this paper, a Global Positioning System (GPS) guided spinning projectile known as the Autonomous Naval Support Round (ANSR) is proposed for development by the US Navy that utilizes the GPS and a gyro-less inertial measurement unit (AO IMU) for guidance and navigation purposes.
Journal ArticleDOI
A Nonlinear Program for Angular-Velocity Estimation From Centripetal-Acceleration Measurements
TL;DR: In this paper, the authors present an algorithm for the estimation of the rigid-body angular velocity from the centripetal components of the accelerations measured by the array of accelerometers.
Proceedings ArticleDOI
Evaluation of Two Guidance Laws for Controlling the Impact Flight Path Angle of a Naval Gun Launched Spinning Projectile
TL;DR: In this paper, two guidance laws, the Generalized Explicit (GENEX) and the Forward Integration of Terminal States (FITS), are evaluated for controlling the impact flight path angle (IFPA) of a naval five-inch gun launched GPS guided rocket assisted spinning projectile.
References
More filters
ReportDOI
Free flight motion of symmetric missiles
TL;DR: In this paper, the linearized angular motion of a symmetric missile is developed in some detail with some consideration of the rolling motion, drag, aerodynamic jump and the effect of varying coefficients.
Related Papers (5)
On the kinematics of the head using linear acceleration measurements
Clifford C. Chou,S. C. Sinha +1 more