Smart Mortar Missile Attitude Detection Based on the Algorithm that Takes Advantage of Artificial Neural Networks

Głębocki, R.; Vogt, R.; Żugaj, Marcin

doi:10.2514/6.2006-6703

Cited by 3 publications

(2 citation statements)

References 6 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…The objective was to measure the trajectory deflection [1]. A unique guidance and control strategy that enables precision and trajectory shaping with reduced sensor and actuator needs was also introduced [2,3].…”

Section: Introductionmentioning

confidence: 99%

Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control

Xiao

Tang

Guo

et al. 2016

International Journal of Aerospace Engineering

View full text Add to dashboard Cite

Random disturbance factors would lead to the variation of target acquisition point during the long distance flight. To acquire a high target acquisition probability and improve the impact precision, missiles should be guided to an appropriate target acquisition position with certain attitude angles and line-of-sight (LOS) angle rate. This paper has presented a new midcourse guidance law considering the influences of random disturbances, detection distance restraint, and target acquisition probability with Monte Carlo simulation. Detailed analyses of the impact points on the ground and the random distribution of the target acquisition position in the 3D space are given to get the appropriate attitude angles and the end position for the midcourse guidance. Then, a new formulation biased proportional navigation (BPN) guidance law with angular constraint and LOS angle rate control has been derived to ensure the tracking ability when attacking the maneuvering target. Numerical simulations demonstrates that, compared with the proportional navigation guidance (PNG) law and the near-optimal spatial midcourse guidance (NSMG) law, BPN guidance law demonstrates satisfactory performances and can meet both the midcourse terminal angular constraint and the LOS angle rate requirement.

show abstract

Section: Introductionmentioning

confidence: 99%

Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control

Xiao

Tang

Guo

et al. 2016

International Journal of Aerospace Engineering

View full text Add to dashboard Cite

show abstract

“…These also produce unknown biases that affect the integration to get the position of the unit. The GPS gives an absolute drift-free position value that can be used to reset the INS solution or may be blended with it by using a mathematical algorithm such as a Kalman filter [1,9]. The angular orientation of the unit may be inferred from the series of position updates from the GPS [10,11].…”

Section: Guidance Impulse Algorithms For Air Bomb Controlmentioning

confidence: 99%

Guidance impulse algorithms for air bomb control

Głębocki¹

2012

Bulletin of the Polish Academy of Sciences: Technical Sciences

View full text Add to dashboard Cite

Abstract. In this paper, some results of research concerning the development of guidance of bombs were presented. The paper presents conceptions of an impulse (gasodynamic) control system, the measurement unit based on IMU/GPS signals and control algorithms based on predicted trajectories. The presented results of simulation research are based on the numerical model of the bomb and real signals from measurement devices.

show abstract

Control System's Algorithms for Gasodynamic Controlled Bombs

Robert

2009

AIAA Guidance, Navigation, and Control Conference

View full text Add to dashboard Cite

Smart Mortar Missile Attitude Detection Based on the Algorithm that Takes Advantage of Artificial Neural Networks

Cited by 3 publications

References 6 publications

Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control

Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control

Guidance impulse algorithms for air bomb control

Control System's Algorithms for Gasodynamic Controlled Bombs

Contact Info

Product

Resources

About