Sentence examples for the guidance problem from inspiring English sources

This paper proposes an alternative formulation of the guidance problem, particularly suitable in autonomous aircraft applications.

The adopted approach to the guidance problem is based on a reference bearing instead of the classical way point.

With this assumption the trajectory problem (also called the guidance problem) and the attitude problem (also called the control problem) can be addressed separately.

Through the A&L guidance problem, the potential of the developed approach is demonstrated.

The COACH system presented above had three significant changes from the previous versions: 1) The use of markerless flocking to track the activity; 2) the use of a partially observable Markov decision process (POMDP) to model the handwashing guidance problem; and 3) the refinement of audio prompts and the addition of video demonstrations.

The approximation capability of artificial neural networks has been applied to the midcourse guidance problem to overcome the difficulty of deriving an on-board guidance algorithm based on optimal control theory.

For the terminal guidance problem of missiles intercepting maneuvering targets in the three-dimensional space, the design of guidance laws for non-decoupling three-dimensional engagement geometry is studied.

The terminal guidance problem for an unpowered lifting reentry vehicle against a stationary target is considered.

In this paper we revisit the micourse guidance problem for maritime area air defense by mixing two contributions (one for mid course guidance law design and one for target allocation).

In particular, a realistic and detailed evaluation of the filter is carried out for the problem of target state estimation in an advanced tactical missile guidance application for analysis in the optimal guidance problem for air-air engagements using only passive sensor (angle-only) information.

After solving the stochastic optimal guidance problem by differential dynamic programming, we point out that the optimal pilot wave guiding the particle's motion is just the wavefunction Ψ t,x), a solution to the Schrödinger equation; meanwhile, the closed-loop guidance system forms a complex state space dynamics for Ψ t,x), from which quantum operators emerge naturally.