Actualization of the Quantomobile Force Balance in the Pitch Plane

2019

AEJ

Self Cite

Introduction: The possibility of energy extraction from the physical vacuum, uncovered in case of potential mastering of the foundations of the theory of Superunification suggested by Leonov, will change the motion mechanics and the pattern of using lift-and-transport machinery if that is equipped with quantum engines (QEs). Purpose of the study: The purpose of the study is to develop a conceptual foundation and a working hypothesis for the operation of unified lift-and-transport machinery with quantum thrust-UQLTM. Methods: The thrust vector is decomposed into orthogonal components. A generalized force balance equation and its modifications are used. Typical modes of QLTM motion are identified. 3D modeling of force balance with velocity sweeping is carried out. 3D models of force balance are developed using Maple software. Images of surfaces with regard to wind resistance and thrust vector dynamics are built. Calculations as well as graphical-and-analytical studies are performed. Results: The paper presents results of calculations with visualization using an example of container transportation from a consolidated terminal to the hold of a container ship with the use of QLTM. Discussion: Existing lift-and-transport machines can be replaced by transport machines equipped with QEs (QLTM), and thus it will be possible to make the area of traditional lift-and-transport machinery movement available. Lifting machines can also be replaced by QLTM. Moreover, several types of lift-andtransport machines as well as transport machines used at warehouses to handle cargo can be replaced by unified QLTM (UQLTM) providing continuous transportation of cargo (without any transshipment using different types of vehicles).

“…As a result of equation 4detalization performed in an analogous way to the way it was performed in other studies (Kotikov, 2019c(Kotikov, , 2019d, we obtain the following:…”

Section: Generalized Qltm Force Balance Equation and Its Modificationsmentioning

confidence: 68%

“…Thrust vector decomposition The three-dimensional thrust vector can be decomposed into unit vectors (Leonov, 2018, Kotikov, 2019c, 2019d:…”

Section: Generalized Mathematical Model Of Qltm Force Balancementioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Unified Quantum Lift-and-Transport Machinery

2019

AEJ

Self Cite

“…The thrust vector in the pitch plane can be decomposed into unit vectors (Leonov, 2018, Kotikov, 2019c:…”

Section: Thrust Vector Decompositionmentioning

confidence: 99%

“…In earlier papers (Kotikov, 2018a(Kotikov, , 2018b(Kotikov, , 2018c(Kotikov, , 2019a(Kotikov, , 2019b(Kotikov, , 2019c, the author described individual aspects of vehicle force balance. Development of a graphical-andanalytical basis to design control over QE thrust and vehicle motion will contribute to further studies on this topic.…”

Section: Introductionmentioning

confidence: 99%

Graphical-and-Analytical Basis for Quantomobile Near-Ground Motion Studies

2019

AEJ

Self Cite

Introduction. Development of a graphical-and-analytical basis to perform optimization calculations for quantomobile motion control will contribute to studies on vehicle creation. Purpose of the study. It is required to develop a methodology for graphical representation of thrust vector realization as a graphical-and-analytical basis for optimization calculations of quantomobile trajectories. Methods. The thrust vector is decomposed into orthogonal components. A generalized quantomobile force balance equation is used. A mode of partial hovering of a vehicle is distinguished as the basic mode of near-ground motion. 2D modeling of force balance for a particular velocity slice is performed. 3D modeling of force balance with velocity sweeping is carried out. 2D and 3D models of force balance are developed using Maple software. Images of surfaces with regard to road and wind resistance with limits to the maximum thrust are built. Examples of calculation as well as graphical-and-analytical studies are provided. Results. A graphical-and-analytical basis for optimization calculations of quantomobile trajectories, changes in QE thrust and corresponding control actions is developed. Results of calculations with visualization are presented using specific examples. Discussion. Development of a program in the graphical environment required combining knowledge of the software tools and programmed field. Development of the quantomobile simulation model as well as its graphical-and-analytical basis in the direction of increasing complexity is the only way. Corresponding development stages are described. Two hypothetical areas for the minimization of sufficient thrust are distinguished: in the middle of vehicle hovering and after its full hovering. It shall be taken into account both in quantomobile takeoff and its near-ground motion with partial hovering.

Quantum Quarrying Lift-and-Transport Machinery (Qqltm)

2020

AEJ